LEMUR 2 ALISIA, 62706
Orbit data source: Space-Track
LEMUR 2 ALISIA, 62706 is a payload satellite owned by Spire (US) in SSO that was launched on Tue, 14 Jan 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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62706 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
7.6 kg wet, 7.6 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.063 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 LEMUR 2 ALISIA
1 62706U 25009DB 26095.46311066 .00011138 00000-0 86104-3 0 9992
2 62706 97.6932 178.1957 0005300 102.1542 258.0276 15.01665099 89245Epoch: 2026-04-05T11:06Z
TLE epoch observation values (Epoch: 2026-04-05T11:06:52.761Z)
Latitude
-0.00003°
Longitude
177.70769°
Altitude
565.584 km
Speed
7.578 km/s
True Right ascension
11h 52m 46s
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
23:41:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.441 km
Perigee altitude
555.088 km
Semi-major axis
6,936.901 km
Eccentricity
0.00053
Inclination
97.6932°
RAAN
178.1957°
Arg. of periapsis
102.1542°
True anomaly
257.9682°
Mean anomaly
258.0276°
Eccentric anomaly
257.9979°
Mean motion
3.7566 °/min
Orbital period
95.83 mins
BSTAR
0.00086104
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Other satellites on launch #9 in the year 2025 (2025-01-14 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 ALISIA 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 | 2026-04-05 18:04:20.816Z | 21.849° NNE | 2026-04-05 18:08:20.816Z | 122.48° SE | 38.987° | 2026-04-05 18:11:20.816Z | 177.461° S |
| 5 mins | 2026-04-06 04:51:20.816Z | 121.047° SE | 2026-04-06 04:53:20.816Z | 79.236° E | 26.401° | 2026-04-06 04:56:20.816Z | 15.824° NNE |
| 4 mins | 2026-04-06 06:27:20.816Z | 241.753° WSW | 2026-04-06 06:28:20.816Z | 260.656° W | 17.72° | 2026-04-06 06:31:20.816Z | 310.672° NW |
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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