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, 0.5 m
Radar Cross Section
0.063 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 LEMUR 2 ALISIA
1 62706U 25009DB 26278.21519301 .00007121 00000-0 51781-3 0 9990
2 62706 97.6899 359.7140 0002323 177.4809 182.6429 15.04133443116699Epoch: 2026-10-05T05:09Z
TLE epoch observation values (Epoch: 2026-10-05T05:09:52.676Z)
Latitude
0.00002°
Longitude
-91.65277°
Altitude
558.837 km
Speed
7.581 km/s
True Right ascension
23h 58m 51s
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
19:25:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
552.776 km
Perigee altitude
549.557 km
Semi-major axis
6,929.303 km
Eccentricity
0.00023
Inclination
97.6899°
RAAN
359.714°
Arg. of periapsis
177.4809°
True anomaly
182.64167°
Mean anomaly
182.6429°
Eccentric anomaly
182.64229°
Mean motion
3.76278 °/min
Orbital period
95.67 mins
BSTAR
0.00051781
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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 | 2026-10-06 05:14:22.286Z | 147.203° SSE | 2026-10-06 05:17:22.286Z | 94.966° ESE | 47.748° | 2026-10-06 05:21:22.286Z | 359.699° N |
| 6 mins | 2026-10-06 18:27:22.286Z | 11.797° NNE | 2026-10-06 18:30:22.286Z | 227.226° WSW | 86.983° | 2026-10-06 18:33:22.286Z | 194.114° SSW |
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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