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: 18 hours ago
TLE from 18 hours ago
0 LEMUR 2 THEFALCONER
1 63264U 25052BG 26212.64543528 .00003981 00000-0 34502-3 0 9993
2 63264 97.6796 104.2866 0002071 148.9471 211.1874 14.97656730 75349Epoch: 2026-07-31T15:29Z
TLE epoch observation values (Epoch: 2026-07-31T15:29:25.608Z)
Latitude
-0°
Longitude
-77.33873°
Altitude
578.423 km
Speed
7.571 km/s
True Right ascension
06h 57m 08s
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
23:01:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.585 km
Perigee altitude
569.707 km
Semi-major axis
6,949.283 km
Eccentricity
0.00021
Inclination
97.6796°
RAAN
104.2866°
Arg. of periapsis
148.9471°
True anomaly
211.17511°
Mean anomaly
211.1874°
Eccentric anomaly
211.18126°
Mean motion
3.74656 °/min
Orbital period
96.09 mins
BSTAR
0.00034502
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-01 17:16:51.176Z | 197.321° SSW | 2026-08-01 17:18:51.176Z | 241.216° WSW | 33.981° | 2026-08-01 17:22:51.176Z | 332.689° NNW |
| 5 mins | 2026-08-02 04:57:51.176Z | 53.746° ENE | 2026-08-02 04:59:51.176Z | 93.972° ESE | 22.609° | 2026-08-02 05:02:51.176Z | 147.718° SSE |
| 5 mins | 2026-08-02 06:32:51.176Z | 333.122° NNW | 2026-08-02 06:34:51.176Z | 294.872° NW | 22.077° | 2026-08-02 06:37:51.176Z | 240.839° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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