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.
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66768 intel report (Beta)
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Identifier
Orbit
Country
USRelated 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)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.063 m²
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 LEMUR-2-TEODOR
1 66768U 25276DG 26092.63792078 .00008240 00000-0 38327-3 0 9996
2 66768 97.4189 167.6047 0002197 86.8758 273.2728 15.20207906 18962Epoch: 2026-04-02T15:18Z
TLE epoch observation values (Epoch: 2026-04-02T15:18:36.355Z)
Latitude
-0.00007°
Longitude
106.9697°
Altitude
508.217 km
Speed
7.61 km/s
True Right ascension
11h 10m 25s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
08:07:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.691 km
Perigee altitude
500.667 km
Semi-major axis
6,880.316 km
Eccentricity
0.00022
Inclination
97.4189°
RAAN
167.6047°
Arg. of periapsis
86.8758°
True anomaly
273.24766°
Mean anomaly
273.2728°
Eccentric anomaly
273.26023°
Mean motion
3.80304 °/min
Orbital period
94.66 mins
BSTAR
0.00038327
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Other satellites on launch #276 in the year 2025 (2025-11-28 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.LEMUR-2-TEODOR Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-04-03 04:06:02.871Z | 109.097° ESE | 2026-04-03 04:08:02.871Z | 73.138° E | 17.566° | 2026-04-03 04:10:02.871Z | 33.93° NE |
| 4 mins | 2026-04-03 05:40:02.871Z | 220.13° SW | 2026-04-03 05:42:02.871Z | 267.607° W | 23.619° | 2026-04-03 05:44:02.871Z | 311.307° NW |
| 4 mins | 2026-04-03 17:11:02.871Z | 65.647° ENE | 2026-04-03 17:12:02.871Z | 91.626° ESE | 23.725° | 2026-04-03 17:15:02.871Z | 152.172° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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