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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 LEMUR 2 AHMED-ASRAR
1 60576U 24149DN 26235.47039394 .00009438 00000-0 52284-3 0 9999
2 60576 97.6978 321.1486 0003463 115.7391 244.4198 15.14028337110749Epoch: 2026-08-23T11:17Z
TLE epoch observation values (Epoch: 2026-08-23T11:17:22.036Z)
Latitude
0°
Longitude
-179.9592°
Altitude
528.037 km
Speed
7.598 km/s
True Right ascension
21h 24m 35s
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
14:02:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
523.306 km
Perigee altitude
518.527 km
Semi-major axis
6,899.054 km
Eccentricity
0.00035
Inclination
97.6978°
RAAN
321.1486°
Arg. of periapsis
115.7391°
True anomaly
244.38401°
Mean anomaly
244.4198°
Eccentric anomaly
244.40191°
Mean motion
3.78755 °/min
Orbital period
95.05 mins
BSTAR
0.00052284
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-08-24 04:53:39.613Z | 105.212° ESE | 2026-08-24 04:55:39.613Z | 69.418° E | 17.227° | 2026-08-24 04:57:39.613Z | 32.574° NE |
| 5 mins | 2026-08-24 06:27:39.613Z | 214.917° SW | 2026-08-24 06:29:39.613Z | 261.359° W | 25.651° | 2026-08-24 06:32:39.613Z | 321.358° NNW |
| 5 mins | 2026-08-24 18:00:39.613Z | 49.566° ENE | 2026-08-24 18:02:39.613Z | 92.078° ESE | 23.536° | 2026-08-24 18:05:39.613Z | 151.261° SSE |
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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