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 26166.71920446 .00005229 00000-0 42418-3 0 9994
2 63395 97.6898 60.3451 0006903 61.6947 298.4972 15.00073642 68547Epoch: 2026-06-15T17:15Z
TLE epoch observation values (Epoch: 2026-06-15T17:15:39.265Z)
Latitude
-0.00003°
Longitude
-102.57006°
Altitude
567.439 km
Speed
7.579 km/s
True Right ascension
04h 01m 22s
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
14:49:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
568.466 km
Perigee altitude
558.882 km
Semi-major axis
6,941.811 km
Eccentricity
0.00069
Inclination
97.6898°
RAAN
60.3451°
Arg. of periapsis
61.6947°
True anomaly
298.42765°
Mean anomaly
298.4972°
Eccentric anomaly
298.46243°
Mean motion
3.75262 °/min
Orbital period
95.93 mins
BSTAR
0.00042418
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-16 05:03:04.137Z | 47.458° ENE | 2026-06-16 05:06:04.137Z | 106.866° ESE | 22.151° | 2026-06-16 05:08:04.137Z | 142.843° SSE |
| 4 mins | 2026-06-16 06:39:04.137Z | 322.808° NNW | 2026-06-16 06:40:04.137Z | 302.439° NW | 21.363° | 2026-06-16 06:43:04.137Z | 244.375° WSW |
| 5 mins | 2026-06-16 17:25:04.137Z | 206.838° SW | 2026-06-16 17:27:04.137Z | 266.793° W | 33.084° | 2026-06-16 17:30:04.137Z | 328.747° 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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