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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 LEMUR-2-TEODOR
1 66768U 25276DG 26192.71735336 .00003149 00000-0 14384-3 0 9990
2 66768 97.4147 266.1085 0002273 90.9117 269.2380 15.21313893 34177Epoch: 2026-07-11T17:12Z
TLE epoch observation values (Epoch: 2026-07-11T17:12:59.330Z)
Latitude
0.00006°
Longitude
78.23472°
Altitude
504.989 km
Speed
7.612 km/s
True Right ascension
17h 44m 26s
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
19:41:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.404 km
Perigee altitude
497.278 km
Semi-major axis
6,876.978 km
Eccentricity
0.00023
Inclination
97.4147°
RAAN
266.1085°
Arg. of periapsis
90.9117°
True anomaly
269.21196°
Mean anomaly
269.238°
Eccentric anomaly
269.22498°
Mean motion
3.80581 °/min
Orbital period
94.59 mins
BSTAR
0.00014384
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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 | 2026-07-12 17:27:54.415Z | 29.307° NE | 2026-07-12 17:30:54.415Z | 114.789° SE | 35.103° | 2026-07-12 17:33:54.415Z | 172.609° S |
| 4 mins | 2026-07-13 05:39:54.415Z | 221.837° SW | 2026-07-13 05:41:54.415Z | 270.226° WNW | 23.246° | 2026-07-13 05:43:54.415Z | 312.382° NW |
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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