LEMUR 2 THEFALCONER, 63264
Orbit data source: Space-Track
LEMUR 2 THEFALCONER, 63264 is a payload satellite owned by Spire (US) in SSO that was launched on Sat, 15 Mar 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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63264 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 LEMUR 2 THEFALCONER
1 63264U 25052BG 26118.28721538 .00003765 00000-0 33190-3 0 9999
2 63264 97.6914 11.4795 0002438 135.3313 224.8105 14.97032547 61227Epoch: 2026-04-28T06:53Z
TLE epoch observation values (Epoch: 2026-04-28T06:53:35.408Z)
Latitude
-0.0001°
Longitude
51.81729°
Altitude
580.325 km
Speed
7.57 km/s
True Right ascension
00h 45m 55s
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
20:47:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
574.775 km
Perigee altitude
571.385 km
Semi-major axis
6,951.217 km
Eccentricity
0.00024
Inclination
97.6914°
RAAN
11.4795°
Arg. of periapsis
135.3313°
True anomaly
224.79081°
Mean anomaly
224.8105°
Eccentric anomaly
224.80066°
Mean motion
3.745 °/min
Orbital period
96.13 mins
BSTAR
0.0003319
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Other satellites on launch #52 in the year 2025 (2025-03-15 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 THEFALCONER 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-04-28 16:38:05.226Z | 154.942° SSE | 2026-04-28 16:42:05.226Z | 68.776° E | 41.329° | 2026-04-28 16:45:05.226Z | 357.587° N |
| 6 mins | 2026-04-29 05:56:05.226Z | 0.143° NNE | 2026-04-29 05:58:05.226Z | 301.279° NW | 42.233° | 2026-04-29 06:02:05.226Z | 203.202° SW |
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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