Showing default

LEMUR 2 STELLA, 60533

Orbit data source: Space-Track

LEMUR 2 STELLA, 60533 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
60533, 2024-149BT
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, Medium (>0.1 m² and < 1m²)

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

TLE from 18 hours ago
0 LEMUR 2 STELLA
1 60533U 24149BT  25286.93711809  .00015691  00000-0  11161-2 0  9992
2 60533  97.6947   4.2819 0001953 121.6357 238.5059 15.04740868 63372
Epoch: 2025-10-13T22:29Z
TLE epoch observation values (Epoch: 2025-10-13T22:29:27.002Z)
Latitude
-0.00013°
Longitude
4.18667°
Altitude
556.07 km
Speed
7.583 km/s
True Right ascension
00h 17m 07s
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
10:41:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
550.653 km
Perigee altitude
547.947 km
Semi-major axis
6,927.437 km
Eccentricity
0.0002
Inclination
97.6947°
RAAN
4.2819°
Arg. of periapsis
121.6357°
True anomaly
238.48682°
Mean anomaly
238.5059°
Eccentric anomaly
238.49636°
Mean motion
3.7643 °/min
Orbital period
95.64 mins
BSTAR
0.0011161
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
|