Showing default

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.

Loading next visibility...
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 (1 year 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, Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago
0 LEMUR 2 MARHISYAM
1 60536U 24149BW  25340.48973701  .00022430  00000-0  15279-2 0  9990
2 60536  97.7061  57.9118 0003423  71.5214 288.6384 15.06274000 71423
Epoch: 2025-12-06T11:45Z
TLE epoch observation values (Epoch: 2025-12-06T11:45:13.277Z)
Latitude
-0.0001°
Longitude
166.08976°
Altitude
549.904 km
Speed
7.587 km/s
True Right ascension
03h 51m 38s
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
04:05:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
546.965 km
Perigee altitude
542.225 km
Semi-major axis
6,922.732 km
Eccentricity
0.00034
Inclination
97.7061°
RAAN
57.9118°
Arg. of periapsis
71.5214°
True anomaly
288.60123°
Mean anomaly
288.6384°
Eccentric anomaly
288.61981°
Mean motion
3.76814 °/min
Orbital period
95.54 mins
BSTAR
0.0015279
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|