Showing default

LEMUR 2 SIERRINI, 60579

Orbit data source: Space-Track

LEMUR 2 SIERRINI, 60579 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.

Loading next visibility...
Identifier
60579, 2024-149DR
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: 19 hours ago

TLE from 19 hours ago
0 LEMUR 2 SIERRINI
1 60579U 24149DR  25340.47182920  .00022337  00000-0  15350-2 0  9997
2 60579  97.7021  57.7732 0006992 111.6068 248.5905 15.05932325 71405
Epoch: 2025-12-06T11:19Z
TLE epoch observation values (Epoch: 2025-12-06T11:19:26.042Z)
Latitude
0.00004°
Longitude
172.4156°
Altitude
553.479 km
Speed
7.584 km/s
True Right ascension
03h 51m 05s
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
04:04:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
550.484 km
Perigee altitude
540.802 km
Semi-major axis
6,923.78 km
Eccentricity
0.0007
Inclination
97.7021°
RAAN
57.7732°
Arg. of periapsis
111.6068°
True anomaly
248.51593°
Mean anomaly
248.5905°
Eccentric anomaly
248.55321°
Mean motion
3.76728 °/min
Orbital period
95.56 mins
BSTAR
0.001535
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
|