TELKOM 3S, 41944
Orbit data source: Space-Track
TELKOM 3S, 41944 is a payload satellite owned by Telkom (ID) in GEO that was launched on Tue, 14 Feb 2017 UTC via an ARIANE 5ECA 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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41944 intel report (Beta)
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Identifier
Orbit
Country
ID / INDORelated business
Manufacturer
Thales Alenia
Mission
Operational Commercial Communications
Bus & Motor
SPACEBUS 4000B2, S400
Mass
3,500 kg wet, ~2,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 18.5 m
Radar Cross Section
31.794 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 TELKOM 3S
1 41944U 17007A 26149.45704931 .00000000 00000-0 00000+0 0 9991
2 41944 0.0159 343.2594 0002667 95.1388 91.1133 1.00267083 33959Epoch: 2026-05-29T10:58Z
TLE epoch observation values (Epoch: 2026-05-29T10:58:09.060Z)
Latitude
-0.01273°
Longitude
118.01258°
Altitude
35,787.656 km
Speed
3.075 km/s
True Right ascension
11h 18m 08s
True Declination
0° 00' 46"
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
01:50:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,800.229 km
Perigee altitude
35,777.738 km
Semi-major axis
42,167.121 km
Eccentricity
0.00027
Inclination
0.0159°
RAAN
343.2594°
Arg. of periapsis
95.1388°
True anomaly
91.14386°
Mean anomaly
91.1133°
Eccentric anomaly
91.12858°
Mean motion
0.25066 °/min
Orbital period
1,436.22 mins
BSTAR
0
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Other satellites on launch #7 in the year 2017 (2017-02-14 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.TELKOM 3S 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. |
|---|---|---|---|---|---|---|---|
| TELKOM 3S is likely not visible in the next few days. |
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41944 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 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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