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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Edit Public Description
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: 8 hours ago
TLE from 8 hours ago
0 LEMUR 2 ALISIA
1 62706U 25009DB 25286.27200752 .00015016 00000-0 12817-2 0 9999
2 62706 97.7319 5.4166 0000783 48.6424 311.4866 14.97786455 63135Epoch: 2025-10-13T06:31Z
TLE epoch observation values (Epoch: 2025-10-13T06:31:41.449Z)
Latitude
0.00002°
Longitude
-114.58328°
Altitude
576.427 km
Speed
7.573 km/s
True Right ascension
00h 21m 39s
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
08:55:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
571.291 km
Perigee altitude
570.203 km
Semi-major axis
6,948.884 km
Eccentricity
0.00008
Inclination
97.7319°
RAAN
5.4166°
Arg. of periapsis
48.6424°
True anomaly
311.47988°
Mean anomaly
311.4866°
Eccentric anomaly
311.48324°
Mean motion
3.74689 °/min
Orbital period
96.08 mins
BSTAR
0.0012817
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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 | 2025-10-13 18:18:29.983Z | 10.868° NNE | 2025-10-13 18:22:29.983Z | 232.936° WSW | 44.657° | 2025-10-13 18:25:29.983Z | 196.04° SSW |
| 5 mins | 2025-10-14 05:07:29.983Z | 139.333° SSE | 2025-10-14 05:09:29.983Z | 73.203° E | 38.73° | 2025-10-14 05:12:29.983Z | 1.208° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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