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 (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, Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 LEMUR 2 MARHISYAM
1 60536U 24149BW  26087.17165942  .00014672  00000-0  91858-3 0  9992
2 60536  97.6895 169.7457 0002705  67.7778 292.3737 15.09485770 88253
Epoch: 2026-03-28T04:07Z
TLE epoch observation values (Epoch: 2026-03-28T04:07:11.373Z)
Latitude
-0.00008°
Longitude
-77.6474°
Altitude
540.126 km
Speed
7.593 km/s
True Right ascension
11h 18m 58s
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
16:01:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
536.632 km
Perigee altitude
532.892 km
Semi-major axis
6,912.899 km
Eccentricity
0.00027
Inclination
97.6895°
RAAN
169.7457°
Arg. of periapsis
67.7778°
True anomaly
292.34503°
Mean anomaly
292.3737°
Eccentric anomaly
292.35937°
Mean motion
3.77618 °/min
Orbital period
95.33 mins
BSTAR
0.00091858
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
|