TELKOMSAT 113BT, 58995
Orbit data source: Space-Track
TELKOMSAT 113BT, 58995 is a payload satellite owned by Telkom (ID) in GEO that was launched on Tue, 20 Feb 2024 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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58995 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / INDORelated business
Manufacturer
Thales Alenia
Mission
Operational Commercial Communications
Bus & Motor
SPACEBUS 4000B2, S400
Mass
4,000 kg wet, ~2,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 15.0 m
Radar Cross Section
48.465 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 TELKOMSAT 113BT
1 58995U 24035A 25322.47113719 -.00000339 00000-0 00000+0 0 9992
2 58995 0.0457 97.2694 0001277 145.5115 97.5674 1.00271087 6471Epoch: 2025-11-18T11:18Z
TLE epoch observation values (Epoch: 2025-11-18T11:18:26.253Z)
Latitude
0.00786°
Longitude
112.96624°
Altitude
35,786.999 km
Speed
3.075 km/s
True Right ascension
22h 41m 19s
True Declination
0° 00' 28"
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
08:54:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,793.246 km
Perigee altitude
35,782.476 km
Semi-major axis
42,165.998 km
Eccentricity
0.00013
Inclination
0.0457°
RAAN
97.2694°
Arg. of periapsis
145.5115°
True anomaly
97.58191°
Mean anomaly
97.5674°
Eccentric anomaly
97.57465°
Mean motion
0.25067 °/min
Orbital period
1,436.16 mins
BSTAR
0
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Other satellites on launch #35 in the year 2024 (2024-02-20 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.TELKOMSAT 113BT 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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| TELKOMSAT 113BT is likely not visible in the next few days. |
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58995 neighbors
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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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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