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: 16 hours ago
TLE from 16 hours ago
0 LEMUR 2 THEFALCONER
1 63264U 25052BG 26306.50815325 .00001378 00000-0 12189-3 0 9994
2 63264 97.6671 196.5235 0000740 190.7751 169.3456 14.97909923 89397Epoch: 2026-11-02T12:11Z
TLE epoch observation values (Epoch: 2026-11-02T12:11:44.440Z)
Latitude
-0.00001°
Longitude
-28.19583°
Altitude
576.914 km
Speed
7.572 km/s
True Right ascension
13h 06m 05s
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
00:22:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
570.876 km
Perigee altitude
569.848 km
Semi-major axis
6,948.499 km
Eccentricity
0.00007
Inclination
97.6671°
RAAN
196.5235°
Arg. of periapsis
190.7751°
True anomaly
169.34717°
Mean anomaly
169.3456°
Eccentric anomaly
169.34638°
Mean motion
3.7472 °/min
Orbital period
96.07 mins
BSTAR
0.00012189
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-03 04:48:41.207Z | 48.734° ENE | 2026-11-03 04:51:41.207Z | 100.407° ESE | 20.481° | 2026-11-03 04:53:41.207Z | 134.99° SE |
| 5 mins | 2026-11-03 06:24:41.207Z | 332.5° NNW | 2026-11-03 06:26:41.207Z | 286.782° WNW | 28.775° | 2026-11-03 06:29:41.207Z | 232.914° WSW |
| 6 mins | 2026-11-03 17:11:41.207Z | 195.92° SSW | 2026-11-03 17:13:41.207Z | 256.557° W | 50.551° | 2026-11-03 17:17:41.207Z | 336.868° NNW |
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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