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: 12 hours ago
TLE from 12 hours ago
0 LEMUR-2-TEODOR
1 66768U 25276DG 26141.20607626 .00004179 00000-0 19316-3 0 9992
2 66768 97.4152 215.3948 0001172 124.9441 235.1904 15.20715904 26344Epoch: 2026-05-21T04:56Z
TLE epoch observation values (Epoch: 2026-05-21T04:56:44.988Z)
Latitude
-0.00012°
Longitude
-97.64724°
Altitude
507.232 km
Speed
7.61 km/s
True Right ascension
14h 21m 34s
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
01:44:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.451 km
Perigee altitude
499.839 km
Semi-major axis
6,878.782 km
Eccentricity
0.00012
Inclination
97.4152°
RAAN
215.3948°
Arg. of periapsis
124.9441°
True anomaly
235.17937°
Mean anomaly
235.1904°
Eccentric anomaly
235.18489°
Mean motion
3.80431 °/min
Orbital period
94.63 mins
BSTAR
0.00019316
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-21 18:08:37.615Z | 355.292° N | 2026-05-21 18:11:37.615Z | 264.676° W | 35.57° | 2026-05-21 18:14:37.615Z | 211.834° SW |
| 5 mins | 2026-05-22 04:46:37.615Z | 148.758° SSE | 2026-05-22 04:48:37.615Z | 88.239° E | 40.585° | 2026-05-22 04:51:37.615Z | 358.29° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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