Showing default

LEMUR-2-TEODOR, 66768

Orbit data source: Space-Track

LEMUR-2-TEODOR, 66768 is a payload satellite owned by Spire (US) in SSO that was launched on Fri, 28 Nov 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
66768, 2025-276DG
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)
2025-11-28 (9 months 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: 22 hours ago

TLE from 22 hours ago
0 LEMUR-2-TEODOR
1 66768U 25276DG  26238.16181141  .00005000  00000-0  22392-3 0  9995
2 66768  97.4107 310.8631 0001026 101.7384 258.3967 15.21708761 41089
Epoch: 2026-08-26T03:53Z
TLE epoch observation values (Epoch: 2026-08-26T03:53:00.505Z)
Latitude
-0.00006°
Longitude
-81.80777°
Altitude
503.921 km
Speed
7.612 km/s
True Right ascension
20h 43m 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
17:11:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.355 km
Perigee altitude
496.944 km
Semi-major axis
6,875.787 km
Eccentricity
0.0001
Inclination
97.4107°
RAAN
310.8631°
Arg. of periapsis
101.7384°
True anomaly
258.38518°
Mean anomaly
258.3967°
Eccentric anomaly
258.39094°
Mean motion
3.8068 °/min
Orbital period
94.57 mins
BSTAR
0.00022392
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
|