LEMUR 2 STELLA, 60533
Orbit data source: Space-Track
LEMUR 2 STELLA, 60533 is a payload satellite owned by Spire (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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60533 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
7.6 kg wet, 7.6 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.063 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 LEMUR 2 STELLA
1 60533U 24149BT 26083.97128112 .00011833 00000-0 73426-3 0 9998
2 60533 97.6748 166.1786 0000970 103.9201 256.2136 15.09867134 87786Epoch: 2026-03-24T23:18Z
TLE epoch observation values (Epoch: 2026-03-24T23:18:38.688Z)
Latitude
-0.00002°
Longitude
-5.92388°
Altitude
539.834 km
Speed
7.592 km/s
True Right ascension
11h 04m 42s
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
21:57:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
534.267 km
Perigee altitude
532.926 km
Semi-major axis
6,911.734 km
Eccentricity
0.0001
Inclination
97.6748°
RAAN
166.1786°
Arg. of periapsis
103.9201°
True anomaly
256.20281°
Mean anomaly
256.2136°
Eccentric anomaly
256.2082°
Mean motion
3.77714 °/min
Orbital period
95.31 mins
BSTAR
0.00073426
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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.LEMUR 2 STELLA 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-03-25 17:23:57.759Z | 60.306° ENE | 2026-03-25 17:25:57.759Z | 97.51° ESE | 17.346° | 2026-03-25 17:27:57.759Z | 132.504° SE |
| 5 mins | 2026-03-25 18:57:57.759Z | 339.55° N | 2026-03-25 18:59:57.759Z | 298.211° NW | 25.447° | 2026-03-25 19:02:57.759Z | 234.38° WSW |
| 6 mins | 2026-03-26 05:39:57.759Z | 183.351° SSW | 2026-03-26 05:41:57.759Z | 225.821° WSW | 39.878° | 2026-03-26 05:45:57.759Z | 339.935° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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