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: 11 hours ago
TLE from 11 hours ago
0 LEMUR 2 AHMED-ASRAR
1 60576U 24149DN 26296.05351331 .00013878 00000-0 74224-3 0 9999
2 60576 97.6962 22.4254 0000629 267.4428 92.6731 15.15184587119918Epoch: 2026-10-23T01:17Z
TLE epoch observation values (Epoch: 2026-10-23T01:17:03.549Z)
Latitude
-0.00012°
Longitude
-28.31895°
Altitude
523.514 km
Speed
7.601 km/s
True Right ascension
01h 29m 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
07:52:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
517.837 km
Perigee altitude
516.969 km
Semi-major axis
6,895.54 km
Eccentricity
0.00006
Inclination
97.6962°
RAAN
22.4254°
Arg. of periapsis
267.4428°
True anomaly
92.6803°
Mean anomaly
92.6731°
Eccentric anomaly
92.6767°
Mean motion
3.79045 °/min
Orbital period
94.98 mins
BSTAR
0.00074224
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-10-23 19:17:28.454Z | 343.602° N | 2026-10-23 19:19:28.454Z | 293.406° NW | 36.476° | 2026-10-23 19:22:28.454Z | 224.506° SW |
| 5 mins | 2026-10-24 05:57:28.454Z | 168.198° S | 2026-10-24 05:59:28.454Z | 318.417° NNW | 85.694° | 2026-10-24 06:02:28.454Z | 347.032° 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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