LEMUR 2 BALTO, 63395
Orbit data source: Space-Track
LEMUR 2 BALTO, 63395 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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63395 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SPIREG/WINGB
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 BALTO
1 63395U 25052BH 26212.67206728 .00004122 00000-0 33191-3 0 9990
2 63395 97.6891 105.7842 0005569 255.3963 104.6643 15.00489370 75433Epoch: 2026-07-31T16:07Z
TLE epoch observation values (Epoch: 2026-07-31T16:07:46.612Z)
Latitude
-0.00009°
Longitude
-85.45488°
Altitude
569.423 km
Speed
7.576 km/s
True Right ascension
07h 03m 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
22:00:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
566.256 km
Perigee altitude
558.525 km
Semi-major axis
6,940.527 km
Eccentricity
0.00056
Inclination
97.6891°
RAAN
105.7842°
Arg. of periapsis
255.3963°
True anomaly
104.72603°
Mean anomaly
104.6643°
Eccentric anomaly
104.69516°
Mean motion
3.75366 °/min
Orbital period
95.91 mins
BSTAR
0.00033191
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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 BALTO 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 16:16:18.190Z | 128.443° SE | 2026-08-01 16:19:18.190Z | 76.766° E | 25.545° | 2026-08-01 16:22:18.190Z | 16.492° NNE |
| 4 mins | 2026-08-01 17:53:18.190Z | 240.787° WSW | 2026-08-01 17:54:18.190Z | 260.388° W | 18.966° | 2026-08-01 17:57:18.190Z | 311.602° NW |
| 6 mins | 2026-08-02 05:31:18.190Z | 29.31° NE | 2026-08-02 05:34:18.190Z | 125.465° SE | 37.277° | 2026-08-02 05:37:18.190Z | 175.649° S |
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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