LEMUR 2 AFFIE-WAUWIE, 66295
Orbit data source: Space-Track
LEMUR 2 AFFIE-WAUWIE, 66295 is a payload satellite owned by Spire (US) in LEO that was launched on Sun, 02 Nov 2025 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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66295 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Communications
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, 0.072 m
Radar Cross Section
0.008 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 LEMUR 2 AFFIE-WAUWIE
1 66295U 25248C 26295.55837628 .00019766 00000-0 64194-3 0 9993
2 66295 45.3919 142.5709 0004206 126.6147 233.5131 15.31693697 54094Epoch: 2026-10-22T13:24Z
TLE epoch observation values (Epoch: 2026-10-22T13:24:03.710Z)
Latitude
-0.00002°
Longitude
-89.43613°
Altitude
472.515 km
Speed
7.63 km/s
True Right ascension
09h 30m 17s
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
15:29:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
475.186 km
Perigee altitude
469.424 km
Semi-major axis
6,850.442 km
Eccentricity
0.00042
Inclination
45.3919°
RAAN
142.5709°
Arg. of periapsis
126.6147°
True anomaly
233.47436°
Mean anomaly
233.5131°
Eccentric anomaly
233.49373°
Mean motion
3.82794 °/min
Orbital period
94.05 mins
BSTAR
0.00064194
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Other satellites on launch #248 in the year 2025 (2025-11-02 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 AFFIE-WAUWIE 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 | 2026-10-22 21:37:51.741Z | 300.739° NW | 2026-10-22 21:40:51.741Z | 353.755° N | 44.848° | 2026-10-22 21:43:51.741Z | 85.566° E |
| 5 mins | 2026-10-22 23:17:51.741Z | 272.566° WNW | 2026-10-22 23:19:51.741Z | 205.51° SW | 43.945° | 2026-10-22 23:22:51.741Z | 141.4° SSE |
| 4 mins | 2026-10-23 16:11:51.741Z | 180.652° SSW | 2026-10-23 16:13:51.741Z | 137.14° SSE | 22.087° | 2026-10-23 16:15:51.741Z | 97.479° ESE |
| 5 mins | 2026-10-23 17:49:51.741Z | 255.524° W | 2026-10-23 17:51:51.741Z | 331.678° NNW | 74.059° | 2026-10-23 17:54:51.741Z | 61.996° ENE |
| 5 mins | 2026-10-23 19:28:51.741Z | 304.16° NW | 2026-10-23 19:30:51.741Z | 1.569° NNE | 33.968° | 2026-10-23 19:33:51.741Z | 61.044° ENE |
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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