ANSER-FLW1, 58019
Orbit data source: Space-Track
ANSER-FLW1, 58019 is a payload satellite owned by INTA (ES) in SSO that was launched on Mon, 09 Oct 2023 UTC via a VEGA launch vehicle from the French Guiana (FRGUI). 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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58019 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, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 4 hours ago
TLE from 4 hours ago
0 ANSER-FLW1
1 58019U 23155D 25308.17324221 .00020800 00000-0 72815-3 0 9995
2 58019 97.5805 26.2586 0002672 139.7672 220.3765 15.29527900114382Epoch: 2025-11-04T04:09Z
TLE epoch observation values (Epoch: 2025-11-04T04:09:28.126Z)
Latitude
-0.00015°
Longitude
-79.77264°
Altitude
481.717 km
Speed
7.624 km/s
True Right ascension
01h 45m 02s
True Declination
0° 00' 01"
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
03:53:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.014 km
Perigee altitude
472.352 km
Semi-major axis
6,852.32 km
Eccentricity
0.00027
Inclination
97.5805°
RAAN
26.2586°
Arg. of periapsis
139.7672°
True anomaly
220.35667°
Mean anomaly
220.3765°
Eccentric anomaly
220.36658°
Mean motion
3.82637 °/min
Orbital period
94.08 mins
BSTAR
0.00072815
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Other satellites on launch #155 in the year 2023 (2023-10-09 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-FLW1 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-04 17:18:05.744Z | 58.552° ENE | 2025-11-04 17:20:05.744Z | 95.012° ESE | 14.976° | 2025-11-04 17:22:05.744Z | 130.702° SE |
| 4 mins | 2025-11-04 18:52:05.744Z | 323.462° NNW | 2025-11-04 18:53:05.744Z | 296.314° NW | 24.519° | 2025-11-04 18:56:05.744Z | 231.511° WSW |
| 5 mins | 2025-11-05 05:25:05.744Z | 169.54° S | 2025-11-05 05:27:05.744Z | 194.427° SSW | 44.508° | 2025-11-05 05:30:05.744Z | 346.315° 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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