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LEMUR 2 MARHISYAM, 60536

Orbit data source: Space-Track

LEMUR 2 MARHISYAM, 60536 is a payload satellite owned by Spire (US) 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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Identifier
60536, 2024-149BW
Orbit
SSO
Country
Flag of USUS
Related 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)
2024-08-16 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
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 & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 LEMUR 2 MARHISYAM
1 60536U 24149BW  26199.77114108  .00005065  00000-0  30038-3 0  9999
2 60536  97.6874 282.8575 0002282  64.0829 296.0636 15.11816351105250
Epoch: 2026-07-18T18:30Z
TLE epoch observation values (Epoch: 2026-07-18T18:30:26.589Z)
Latitude
-0°
Longitude
68.6676°
Altitude
533.039 km
Speed
7.597 km/s
True Right ascension
18h 51m 25s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
18:47:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
529.226 km
Perigee altitude
526.074 km
Semi-major axis
6,905.787 km
Eccentricity
0.00023
Inclination
97.6874°
RAAN
282.8575°
Arg. of periapsis
64.0829°
True anomaly
296.04011°
Mean anomaly
296.0636°
Eccentric anomaly
296.05185°
Mean motion
3.78202 °/min
Orbital period
95.19 mins
BSTAR
0.00030038
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