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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 LEMUR 2 BALTO
1 63395U 25052BH 26074.63599615 .00006313 00000-0 52534-3 0 9998
2 63395 97.6982 329.3829 0001528 355.0560 5.0647 14.99025599 54740Epoch: 2026-03-15T15:15Z
TLE epoch observation values (Epoch: 2026-03-15T15:15:50.067Z)
Latitude
-0.00007°
Longitude
-72.81569°
Altitude
571.901 km
Speed
7.576 km/s
True Right ascension
21h 57m 31s
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
04:03:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
567.973 km
Perigee altitude
565.851 km
Semi-major axis
6,945.049 km
Eccentricity
0.00015
Inclination
97.6982°
RAAN
329.3829°
Arg. of periapsis
355.056°
True anomaly
5.06625°
Mean anomaly
5.0647°
Eccentric anomaly
5.06547°
Mean motion
3.74999 °/min
Orbital period
96 mins
BSTAR
0.00052534
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-03-16 04:40:36.073Z | 62.632° ENE | 2026-03-16 04:42:36.073Z | 93.414° ESE | 13.575° | 2026-03-16 04:44:36.073Z | 123.6° SE |
| 6 mins | 2026-03-16 06:15:36.073Z | 346.247° N | 2026-03-16 06:17:36.073Z | 296.843° NW | 33.429° | 2026-03-16 06:21:36.073Z | 216.766° SW |
| 6 mins | 2026-03-16 17:01:36.073Z | 172.76° S | 2026-03-16 17:04:36.073Z | 285.366° WNW | 44.186° | 2026-03-16 17:07:36.073Z | 343.688° N |
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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