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: 11 hours ago
TLE from 11 hours ago
0 LEMUR 2 BALTO
1 63395U 25052BH 26260.01574972 .00003825 00000-0 30612-3 0 9994
2 63395 97.6667 152.5436 0009258 118.0928 242.1233 15.00739339 82533Epoch: 2026-09-17T00:22Z
TLE epoch observation values (Epoch: 2026-09-17T00:22:40.775Z)
Latitude
-0.00003°
Longitude
150.91466°
Altitude
570.682 km
Speed
7.574 km/s
True Right ascension
10h 10m 10s
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
03:54:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
568.043 km
Perigee altitude
555.193 km
Semi-major axis
6,939.755 km
Eccentricity
0.00093
Inclination
97.6667°
RAAN
152.5436°
Arg. of periapsis
118.0928°
True anomaly
242.02957°
Mean anomaly
242.1233°
Eccentric anomaly
242.07643°
Mean motion
3.75428 °/min
Orbital period
95.89 mins
BSTAR
0.00030612
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-17 16:30:25.661Z | 141.307° SSE | 2026-09-17 16:33:25.661Z | 91.062° ESE | 39.535° | 2026-09-17 16:37:25.661Z | 3.738° NNE |
| 6 mins | 2026-09-18 05:45:25.661Z | 16.254° NNE | 2026-09-18 05:48:25.661Z | 154.048° SSE | 73.832° | 2026-09-18 05:51:25.661Z | 188.875° SSW |
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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