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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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: 21 hours ago
TLE from 21 hours ago
0 ANSER-LS
1 62644U 25009AM 26079.19852706 .00036475 00000-0 94656-3 0 9998
2 62644 97.4048 164.4011 0001888 236.4394 123.6671 15.38897512 65487Epoch: 2026-03-20T04:45Z
TLE epoch observation values (Epoch: 2026-03-20T04:45:52.737Z)
Latitude
-0.00008°
Longitude
-84.80566°
Altitude
453.199 km
Speed
7.64 km/s
True Right ascension
10h 57m 36s
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
06:23:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
447.597 km
Perigee altitude
445.02 km
Semi-major axis
6,824.446 km
Eccentricity
0.00019
Inclination
97.4048°
RAAN
164.4011°
Arg. of periapsis
236.4394°
True anomaly
123.6851°
Mean anomaly
123.6671°
Eccentric anomaly
123.6761°
Mean motion
3.84983 °/min
Orbital period
93.51 mins
BSTAR
0.00094656
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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 | 2026-03-21 05:51:50.067Z | 182.202° SSW | 2026-03-21 05:53:50.067Z | 219.287° SW | 37.962° | 2026-03-21 05:56:50.067Z | 336.781° NNW |
| 4 mins | 2026-03-21 18:47:50.067Z | 342.564° N | 2026-03-21 18:48:50.067Z | 304.525° NW | 36.366° | 2026-03-21 18:51:50.067Z | 212.207° SW |
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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