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LEMUR-2-TEODOR, 66768

Orbit data source: Space-Track

LEMUR-2-TEODOR, 66768 is an American payload satellite 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.

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Identifier
66768, 2025-276DG
Orbit
SSO
Country
Flag of USUS
Related business
None
Manufacturer
Unknown
Mission
Operational Commercial Sigint/Imaging
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2025-11-28 (2 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Trap Box + Cyl, 0.5 m
Radar Cross Section
0.655 m²

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 LEMUR-2-TEODOR
1 66768U 25276DG  26034.63203111  .00008788  00000-0  41867-3 0  9997
2 66768  97.4291 110.5403 0000512 120.3435 239.7851 15.19357812 10151
Epoch: 2026-02-03T15:10Z
TLE epoch observation values (Epoch: 2026-02-03T15:10:07.487Z)
Latitude
0.00001°
Longitude
109.19892°
Altitude
511.047 km
Speed
7.608 km/s
True Right ascension
07h 22m 09s
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
04:08:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.1 km
Perigee altitude
504.396 km
Semi-major axis
6,882.885 km
Eccentricity
0.00005
Inclination
97.4291°
RAAN
110.5403°
Arg. of periapsis
120.3435°
True anomaly
239.78003°
Mean anomaly
239.7851°
Eccentric anomaly
239.78257°
Mean motion
3.80091 °/min
Orbital period
94.71 mins
BSTAR
0.00041867
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