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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 LEMUR 2 ALISIA
1 62706U 25009DB 26171.46486470 .00005856 00000-0 44193-3 0 9991
2 62706 97.6936 253.6125 0002315 189.2638 170.8545 15.02804196100653Epoch: 2026-06-20T11:09Z
TLE epoch observation values (Epoch: 2026-06-20T11:09:24.310Z)
Latitude
0.00004°
Longitude
177.5821°
Altitude
562.898 km
Speed
7.579 km/s
True Right ascension
16h 54m 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
07:21:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
556.86 km
Perigee altitude
553.65 km
Semi-major axis
6,933.392 km
Eccentricity
0.00023
Inclination
97.6936°
RAAN
253.6125°
Arg. of periapsis
189.2638°
True anomaly
170.85872°
Mean anomaly
170.8545°
Eccentric anomaly
170.85661°
Mean motion
3.75945 °/min
Orbital period
95.76 mins
BSTAR
0.00044193
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-21 04:52:49.658Z | 123.719° SE | 2026-06-21 04:55:49.658Z | 57.081° ENE | 25.855° | 2026-06-21 04:57:49.658Z | 18.639° NNE |
| 4 mins | 2026-06-21 06:28:49.658Z | 238.59° WSW | 2026-06-21 06:29:49.658Z | 257.004° W | 17.689° | 2026-06-21 06:32:49.658Z | 308.822° NW |
| 6 mins | 2026-06-21 18:05:49.658Z | 27.963° NE | 2026-06-21 18:08:49.658Z | 121.763° SE | 37.969° | 2026-06-21 18:11:49.658Z | 176.038° S |
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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