ORESAT0.5, 60525
Orbit data source: Space-Track
ORESAT0.5, 60525 is a payload satellite owned by Portland State (US) in SSO that was launched on Fri, 16 Aug 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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60525 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Portland State
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 1.5U, Unknown motor
Mass
2 kg wet, 2 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Ant, 0.3 m
Radar Cross Section
0.040 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 ORESAT0.5
1 60525U 24149BK 26083.96793640 .00019105 00000-0 45249-3 0 9994
2 60525 97.3736 168.8829 0005399 209.2244 150.8701 15.41799657 89481Epoch: 2026-03-24T23:13Z
TLE epoch observation values (Epoch: 2026-03-24T23:13:49.704Z)
Latitude
-0.00012°
Longitude
-2.01217°
Altitude
447.136 km
Speed
7.642 km/s
True Right ascension
11h 15m 31s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
21:57:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
441.413 km
Perigee altitude
434.053 km
Semi-major axis
6,815.87 km
Eccentricity
0.00054
Inclination
97.3736°
RAAN
168.8829°
Arg. of periapsis
209.2244°
True anomaly
150.9002°
Mean anomaly
150.8701°
Eccentric anomaly
150.88515°
Mean motion
3.8571 °/min
Orbital period
93.33 mins
BSTAR
0.00045249
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Other satellites on launch #149 in the year 2024 (2024-08-16 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ORESAT0.5 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-03-25 18:29:05.910Z | 11.576° NNE | 2026-03-25 18:31:05.910Z | 9.822° NNE | 41.88° | 2026-03-25 18:34:05.910Z | 193.329° SSW |
| 4 mins | 2026-03-26 04:59:05.910Z | 106.53° ESE | 2026-03-26 05:00:05.910Z | 82.687° E | 20.765° | 2026-03-26 05:03:05.910Z | 18.205° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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