ANSER-LS, 62644
Orbit data source: Space-Track
ANSER-LS, 62644 is a payload satellite owned by INTA (ES) 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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62644 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
ES / SPNRelated business
Manufacturer
INTA
Mission
Operational Civil Imaging
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 ANSER-LS
1 62644U 25009AM 25354.18684954 .00008737 00000-0 28327-3 0 9992
2 62644 97.4205 73.8781 0001509 198.2276 161.8912 15.32227969 51678Epoch: 2025-12-20T04:29Z
TLE epoch observation values (Epoch: 2025-12-20T04:29:03.800Z)
Latitude
0°
Longitude
-82.40499°
Altitude
473.255 km
Speed
7.629 km/s
True Right ascension
04h 55m 30s
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
15:27:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
467.15 km
Perigee altitude
465.084 km
Semi-major axis
6,844.254 km
Eccentricity
0.00015
Inclination
97.4205°
RAAN
73.8781°
Arg. of periapsis
198.2276°
True anomaly
161.89657°
Mean anomaly
161.8912°
Eccentric anomaly
161.89389°
Mean motion
3.83313 °/min
Orbital period
93.92 mins
BSTAR
0.00028327
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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.ANSER-LS 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 | 2025-12-20 17:35:44.332Z | 47.51° ENE | 2025-12-20 17:37:44.332Z | 83.449° E | 18.471° | 2025-12-20 17:40:44.332Z | 143.358° SSE |
| 4 mins | 2025-12-20 19:09:44.332Z | 324.1° NNW | 2025-12-20 19:11:44.332Z | 277.525° WNW | 19.066° | 2025-12-20 19:13:44.332Z | 241.733° WSW |
| 5 mins | 2025-12-21 05:41:44.332Z | 179.1° S | 2025-12-21 05:43:44.332Z | 217.786° SW | 40.762° | 2025-12-21 05:46:44.332Z | 339.765° 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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