ANSER-FLW2, 58018
Orbit data source: Space-Track
ANSER-FLW2, 58018 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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58018 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-FLW2
1 58018U 23155C 25308.17326182 .00014590 00000-0 51188-3 0 9991
2 58018 97.5748 25.7396 0001306 112.6606 247.4772 15.29536807114384Epoch: 2025-11-04T04:09Z
TLE epoch observation values (Epoch: 2025-11-04T04:09:29.821Z)
Latitude
-0.00001°
Longitude
-80.29874°
Altitude
480.637 km
Speed
7.625 km/s
True Right ascension
01h 42m 57s
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
03:53:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
475.051 km
Perigee altitude
473.262 km
Semi-major axis
6,852.293 km
Eccentricity
0.00013
Inclination
97.5748°
RAAN
25.7396°
Arg. of periapsis
112.6606°
True anomaly
247.46338°
Mean anomaly
247.4772°
Eccentric anomaly
247.47029°
Mean motion
3.82639 °/min
Orbital period
94.08 mins
BSTAR
0.00051188
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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-FLW2 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 17:18:04.223Z | 57.237° ENE | 2025-11-04 17:20:04.223Z | 94.458° ESE | 15.868° | 2025-11-04 17:22:04.223Z | 131.475° SE |
| 4 mins | 2025-11-04 18:52:04.223Z | 322.716° NNW | 2025-11-04 18:53:04.223Z | 296.759° NW | 23.396° | 2025-11-04 18:56:04.223Z | 233.434° WSW |
| 5 mins | 2025-11-05 05:25:04.223Z | 172.449° S | 2025-11-05 05:27:04.223Z | 211.348° SW | 44.025° | 2025-11-05 05:30:04.223Z | 344.586° 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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