Showing default

LEMUR 2 MYNAMEISJEFF, 62712

Orbit data source: Space-Track

LEMUR 2 MYNAMEISJEFF, 62712 is a payload satellite owned by Spire (US) in SSO that was launched on Tue, 14 Jan 2025 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
62712, 2025-009DH
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)
2025-01-14 (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, 0.2 m
Radar Cross Section
0.063 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 LEMUR 2 MYNAMEISJEFF
1 62712U 25009DH  26126.49470284  .00007731  00000-0  57668-3 0  9992
2 62712  97.7295 209.6149 0001397   5.2750 354.8489 15.03142066 71365
Epoch: 2026-05-06T11:52Z
TLE epoch observation values (Epoch: 2026-05-06T11:52:22.325Z)
Latitude
-0.00007°
Longitude
167.16751°
Altitude
559.308 km
Speed
7.582 km/s
True Right ascension
13h 58m 27s
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
05:09:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
555.186 km
Perigee altitude
553.249 km
Semi-major axis
6,932.354 km
Eccentricity
0.00014
Inclination
97.7295°
RAAN
209.6149°
Arg. of periapsis
5.275°
True anomaly
354.84746°
Mean anomaly
354.8489°
Eccentric anomaly
354.84818°
Mean motion
3.7603 °/min
Orbital period
95.74 mins
BSTAR
0.00057668
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
|