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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Identifier
Orbit
Country
TH / 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: 6 hours ago
TLE from 6 hours ago
0 T2V
1 58016U 23155A 26154.47183440 .00001010 00000-0 13475-3 0 9990
2 58016 97.8883 225.6593 0001489 90.6945 269.4439 14.81716484143393Epoch: 2026-06-03T11:19Z
TLE epoch observation values (Epoch: 2026-06-03T11:19:26.492Z)
Latitude
0.00004°
Longitude
163.86894°
Altitude
626.946 km
Speed
7.545 km/s
True Right ascension
15h 02m 38s
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
03:14:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
621.991 km
Perigee altitude
619.907 km
Semi-major axis
6,999.086 km
Eccentricity
0.00015
Inclination
97.8883°
RAAN
225.6593°
Arg. of periapsis
90.6945°
True anomaly
269.42684°
Mean anomaly
269.4439°
Eccentric anomaly
269.43537°
Mean motion
3.70665 °/min
Orbital period
97.12 mins
BSTAR
0.00013475
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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 | 2026-06-03 18:22:10.555Z | 346.799° N | 2026-06-03 18:25:10.555Z | 297.345° NW | 25.926° | 2026-06-03 18:28:10.555Z | 238.519° WSW |
| 4 mins | 2026-06-04 03:42:10.555Z | 93.474° ESE | 2026-06-04 03:44:10.555Z | 59.749° ENE | 16.971° | 2026-06-04 03:46:10.555Z | 29.553° NE |
| 6 mins | 2026-06-04 05:17:10.555Z | 203.007° SW | 2026-06-04 05:20:10.555Z | 278.701° WNW | 31.601° | 2026-06-04 05:23:10.555Z | 328.295° NNW |
| 6 mins | 2026-06-04 17:05:10.555Z | 40.382° NE | 2026-06-04 17:08:10.555Z | 109.175° ESE | 30.197° | 2026-06-04 17:11:10.555Z | 161.244° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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