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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Edit Public Description
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: 18 hours ago
TLE from 18 hours ago
0 LEMUR 2 AHMED-ASRAR
1 60576U 24149DN 25286.90735231 .00014210 00000-0 98250-3 0 9992
2 60576 97.7193 5.6074 0003403 120.0494 240.1070 15.05822509 63419Epoch: 2025-10-13T21:46Z
TLE epoch observation values (Epoch: 2025-10-13T21:46:35.239Z)
Latitude
-0.00007°
Longitude
16.25718°
Altitude
553.22 km
Speed
7.584 km/s
True Right ascension
00h 22m 25s
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
10:38:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
548.337 km
Perigee altitude
543.624 km
Semi-major axis
6,924.117 km
Eccentricity
0.00034
Inclination
97.7193°
RAAN
5.6074°
Arg. of periapsis
120.0494°
True anomaly
240.0732°
Mean anomaly
240.107°
Eccentric anomaly
240.0901°
Mean motion
3.76701 °/min
Orbital period
95.57 mins
BSTAR
0.0009825
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-14 17:29:12.773Z | 41.602° NE | 2025-10-14 17:32:12.773Z | 93.664° ESE | 22.081° | 2025-10-14 17:35:12.773Z | 148.236° SSE |
| 4 mins | 2025-10-14 19:05:12.773Z | 325.953° NNW | 2025-10-14 19:07:12.773Z | 282.913° WNW | 21.039° | 2025-10-14 19:09:12.773Z | 246.342° WSW |
| 6 mins | 2025-10-15 05:48:12.773Z | 195.886° SSW | 2025-10-15 05:51:12.773Z | 279.857° WNW | 33.412° | 2025-10-15 05:54:12.773Z | 332.023° NNW |
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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