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LEMUR-2-DEANANDMAEVE, 66678

Orbit data source: Space-Track

LEMUR-2-DEANANDMAEVE, 66678 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.

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Identifier
66678, 2025-276N
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 (2 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

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 LEMUR-2-DEANANDMAEVE
1 66678U 25276N   26035.09995325  .00009676  00000-0  48195-3 0  9991
2 66678  97.4352 110.8896 0007315 102.2563 257.9491 15.17755995 10218
Epoch: 2026-02-04T02:23Z
TLE epoch observation values (Epoch: 2026-02-04T02:23:55.960Z)
Latitude
0.00002°
Longitude
-59.36496°
Altitude
516.767 km
Speed
7.605 km/s
True Right ascension
07h 23m 33s
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
10:14:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
514.633 km
Perigee altitude
504.556 km
Semi-major axis
6,887.731 km
Eccentricity
0.00073
Inclination
97.4352°
RAAN
110.8896°
Arg. of periapsis
102.2563°
True anomaly
257.86714°
Mean anomaly
257.9491°
Eccentric anomaly
257.90812°
Mean motion
3.7969 °/min
Orbital period
94.81 mins
BSTAR
0.00048195
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