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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Edit Public Description
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: 18 hours ago
TLE from 18 hours ago
0 LEMUR 2 BALTO
1 63395U 25052BH 25286.96671364 .00007653 00000-0 68705-3 0 9995
2 63395 97.7092 178.7539 0003940 101.8701 258.2962 14.95995608 31897Epoch: 2025-10-13T23:12Z
TLE epoch observation values (Epoch: 2025-10-13T23:12:04.058Z)
Latitude
-0.00004°
Longitude
167.97509°
Altitude
582.89 km
Speed
7.569 km/s
True Right ascension
11h 55m 00s
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
11:57:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
579.035 km
Perigee altitude
573.555 km
Semi-major axis
6,954.432 km
Eccentricity
0.00039
Inclination
97.7092°
RAAN
178.7539°
Arg. of periapsis
101.8701°
True anomaly
258.25199°
Mean anomaly
258.2962°
Eccentric anomaly
258.2741°
Mean motion
3.7424 °/min
Orbital period
96.19 mins
BSTAR
0.00068705
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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 | 2025-10-15 04:41:21.957Z | 59.315° ENE | 2025-10-15 04:43:21.957Z | 89.637° E | 14.291° | 2025-10-15 04:45:21.957Z | 121.326° SE |
| 6 mins | 2025-10-15 06:16:21.957Z | 349.099° N | 2025-10-15 06:19:21.957Z | 272.966° WNW | 32.227° | 2025-10-15 06:22:21.957Z | 220.443° SW |
| 6 mins | 2025-10-15 17:04:21.957Z | 177.27° S | 2025-10-15 17:07:21.957Z | 302.835° NW | 42.092° | 2025-10-15 17:10:21.957Z | 342.024° 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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