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: 2 days ago
TLE from 2 days ago
0 LEMUR 2 BALTO
1 63395U 25052BH 26305.48386365 .00004733 00000-0 37468-3 0 9997
2 63395 97.6514 197.3618 0004796 334.7243 25.3746 15.01064721 89356Epoch: 2026-11-01T11:36Z
TLE epoch observation values (Epoch: 2026-11-01T11:36:45.819Z)
Latitude
0°
Longitude
-17.60369°
Altitude
563.661 km
Speed
7.581 km/s
True Right ascension
13h 09m 26s
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
00:23:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
563.941 km
Perigee altitude
557.286 km
Semi-major axis
6,938.751 km
Eccentricity
0.00048
Inclination
97.6514°
RAAN
197.3618°
Arg. of periapsis
334.7243°
True anomaly
25.39816°
Mean anomaly
25.3746°
Eccentric anomaly
25.38638°
Mean motion
3.7551 °/min
Orbital period
95.87 mins
BSTAR
0.00037468
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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 | 2026-11-03 05:46:04.340Z | 13.788° NNE | 2026-11-03 05:50:04.340Z | 166.171° S | 76.283° | 2026-11-03 05:53:04.340Z | 190.58° SSW |
| 6 mins | 2026-11-03 16:33:04.340Z | 135.389° SSE | 2026-11-03 16:35:04.340Z | 91.826° ESE | 41.269° | 2026-11-03 16:39:04.340Z | 2.88° NNE |
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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