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: 20 hours ago
TLE from 20 hours ago
0 LEMUR 2 AHMED-ASRAR
1 60576U 24149DN 26080.19279757 .00013228 00000-0 80286-3 0 9990
2 60576 97.7012 164.5152 0000873 314.3207 45.7951 15.10647573 87278Epoch: 2026-03-21T04:37Z
TLE epoch observation values (Epoch: 2026-03-21T04:37:37.710Z)
Latitude
0.00005°
Longitude
-83.60896°
Altitude
536.872 km
Speed
7.594 km/s
True Right ascension
10h 58m 03s
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
05:47:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
531.818 km
Perigee altitude
530.612 km
Semi-major axis
6,909.352 km
Eccentricity
0.00009
Inclination
97.7012°
RAAN
164.5152°
Arg. of periapsis
314.3207°
True anomaly
45.80227°
Mean anomaly
45.7951°
Eccentric anomaly
45.79869°
Mean motion
3.77909 °/min
Orbital period
95.26 mins
BSTAR
0.00080286
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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 | 2026-03-22 04:37:57.513Z | 102.618° ESE | 2026-03-22 04:39:57.513Z | 66.726° ENE | 17.023° | 2026-03-22 04:41:57.513Z | 31.451° NE |
| 5 mins | 2026-03-22 06:11:57.513Z | 212.788° SW | 2026-03-22 06:13:57.513Z | 258.845° W | 26.704° | 2026-03-22 06:16:57.513Z | 321.327° NNW |
| 5 mins | 2026-03-22 17:46:57.513Z | 55.145° ENE | 2026-03-22 17:48:57.513Z | 102.656° ESE | 24.041° | 2026-03-22 17:51:57.513Z | 154.829° 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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