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, 0.1 m
Radar Cross Section
0.008 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 LEMUR 2 AFFIE-WAUWIE
1 66295U 25248C 26242.56305966 .00018575 00000-0 64213-3 0 9990
2 66295 45.3904 71.2172 0006934 171.4987 188.6022 15.29699547 45973Epoch: 2026-08-30T13:30Z
TLE epoch observation values (Epoch: 2026-08-30T13:30:48.354Z)
Latitude
0.00001°
Longitude
-110.24111°
Altitude
481.451 km
Speed
7.624 km/s
True Right ascension
04h 44m 52s
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
19:56:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
483.009 km
Perigee altitude
473.501 km
Semi-major axis
6,856.392 km
Eccentricity
0.00069
Inclination
45.3904°
RAAN
71.2172°
Arg. of periapsis
171.4987°
True anomaly
188.59033°
Mean anomaly
188.6022°
Eccentric anomaly
188.59626°
Mean motion
3.82296 °/min
Orbital period
94.17 mins
BSTAR
0.00064213
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-08-31 14:45:44.520Z | 182.106° SSW | 2026-08-31 14:47:44.520Z | 147.806° SSE | 17.379° | 2026-08-31 14:49:44.520Z | 107.853° ESE |
| 6 mins | 2026-08-31 16:23:44.520Z | 246.531° WSW | 2026-08-31 16:26:44.520Z | 55.496° ENE | 43.275° | 2026-08-31 16:29:44.520Z | 64.927° ENE |
| 4 mins | 2026-08-31 18:03:44.520Z | 306.447° NW | 2026-08-31 18:05:44.520Z | 12.53° NNE | 29.316° | 2026-08-31 18:07:44.520Z | 54.404° ENE |
| 5 mins | 2026-08-31 19:42:44.520Z | 317.735° NNW | 2026-08-31 19:44:44.520Z | 30.879° NE | 32.946° | 2026-08-31 19:47:44.520Z | 84.35° E |
| 5 mins | 2026-08-31 21:20:44.520Z | 283.72° WNW | 2026-08-31 21:22:44.520Z | 236.321° WSW | 39.421° | 2026-08-31 21:25:44.520Z | 133.856° SE |
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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