LEMUR 2 AHMED-ASRAR, 60576
Orbit data source: Space-Track
LEMUR 2 AHMED-ASRAR, 60576 is an American payload satellite 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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60576 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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 LEMUR 2 AHMED-ASRAR
1 60576U 24149DN 26084.49808691 .00012045 00000-0 72889-3 0 9998
2 60576 97.7008 168.8479 0000614 281.0981 79.0179 15.10779735 87924Epoch: 2026-03-25T11:57Z
TLE epoch observation values (Epoch: 2026-03-25T11:57:14.709Z)
Latitude
-0.00002°
Longitude
166.57609°
Altitude
536.809 km
Speed
7.594 km/s
True Right ascension
11h 15m 23s
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
23:16:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
531.236 km
Perigee altitude
530.387 km
Semi-major axis
6,908.949 km
Eccentricity
0.00006
Inclination
97.7008°
RAAN
168.8479°
Arg. of periapsis
281.0981°
True anomaly
79.02481°
Mean anomaly
79.0179°
Eccentric anomaly
79.02135°
Mean motion
3.77942 °/min
Orbital period
95.25 mins
BSTAR
0.00072889
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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 AHMED-ASRAR 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-25 18:51:56.616Z | 356.762° N | 2026-03-25 18:54:56.616Z | 306.177° NW | 32.661° | 2026-03-25 18:58:56.616Z | 216.419° SW |
| 5 mins | 2026-03-26 05:34:56.616Z | 165.091° S | 2026-03-26 05:36:56.616Z | 135.604° SSE | 44.878° | 2026-03-26 05:39:56.616Z | 348.515° N |
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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