T2V, 58016
Orbit data source: Space-Track
T2V, 58016 is a payload satellite owned by GISTDA (TH) 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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58016 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / THAIRelated business
Manufacturer
Astrium/Toulouse
Mission
Operational Civil Imaging
Bus & Motor
ASTROBUS-S, Unknown motor
Mass
417 kg wet, 417 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 2.6 m
Radar Cross Section
3.630 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 T2V
1 58016U 23155A 25307.82359532 .00001277 00000-0 16856-3 0 9996
2 58016 97.8849 16.9937 0001330 87.3188 272.8177 14.81736325112057Epoch: 2025-11-03T19:45Z
TLE epoch observation values (Epoch: 2025-11-03T19:45:58.635Z)
Latitude
-0.00005°
Longitude
37.17996°
Altitude
626.827 km
Speed
7.545 km/s
True Right ascension
01h 07m 58s
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
21:09:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
621.817 km
Perigee altitude
619.956 km
Semi-major axis
6,999.024 km
Eccentricity
0.00013
Inclination
97.8849°
RAAN
16.9937°
Arg. of periapsis
87.3188°
True anomaly
272.80248°
Mean anomaly
272.8177°
Eccentric anomaly
272.81009°
Mean motion
3.7067 °/min
Orbital period
97.12 mins
BSTAR
0.00016856
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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.T2V 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-04 04:00:25.647Z | 125.66° SE | 2025-11-04 04:03:25.647Z | 77.381° E | 25.217° | 2025-11-04 04:06:25.647Z | 19.094° NNE |
| 5 mins | 2025-11-04 05:37:25.647Z | 221.115° SW | 2025-11-04 05:39:25.647Z | 254.993° W | 21.581° | 2025-11-04 05:42:25.647Z | 309.751° NW |
| 6 mins | 2025-11-04 17:25:25.647Z | 25.896° NE | 2025-11-04 17:28:25.647Z | 135.187° SSE | 40.276° | 2025-11-04 17:31:25.647Z | 180.346° SSW |
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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