TELEOS 2, 56310
Orbit data source: Space-Track
TELEOS 2, 56310 is a payload satellite owned by AgilSpace (SG) in LEO that was launched on Sat, 22 Apr 2023 UTC via a PSLV launch vehicle from the Sirharikota (SRI). 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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Identifier
Orbit
Country
SG / SINGRelated business
Manufacturer
STE Sat Sys
Mission
Operational Commercial Radar Imaging
Bus & Motor
SS-400, Unknown motor
Mass
741 kg wet, 741 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Hex Cyl + 4 Pan, 2.0 m
Radar Cross Section
6.467 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 TELEOS 2
1 56310U 23057C 26172.55500589 .00000686 00000-0 -11107-6 0 9994
2 56310 9.9868 172.3778 0000182 297.1616 62.8579 14.96376406173458Epoch: 2026-06-21T13:19Z
TLE epoch observation values (Epoch: 2026-06-21T13:19:12.508Z)
Latitude
-0.00001°
Longitude
62.82204°
Altitude
575.085 km
Speed
7.576 km/s
True Right ascension
11h 29m 30s
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
21:41:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.284 km
Perigee altitude
584.031 km
Semi-major axis
6,962.295 km
Eccentricity
0.00002
Inclination
9.9868°
RAAN
172.3778°
Arg. of periapsis
297.1616°
True anomaly
62.85976°
Mean anomaly
62.8579°
Eccentric anomaly
62.85883°
Mean motion
3.73607 °/min
Orbital period
96.36 mins
BSTAR
-1.1107e-7
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Other satellites on launch #57 in the year 2023 (2023-04-22 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.TELEOS 2 Visibility
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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. |
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| TELEOS 2 is likely not visible in the next few days. |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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