ANIK G1, 39127
Orbit data source: Space-Track
ANIK G1, 39127 is a payload satellite owned by Telesat (Loral) (CA) in GEO that was launched on Mon, 15 Apr 2013 UTC via a PROTON-M/BRIZ-M launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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39127 intel report (Beta)
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Identifier
Orbit
Country
CARelated business
Manufacturer
SS/Loral (MDA)
Mission
Operational Commercial Communications
Bus & Motor
SSL-1300, R-4D-15?
Mass
4,905 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
50.206 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 ANIK G1
1 39127U 13014A 26318.44617122 -.00000062 00000-0 00000+0 0 9996
2 39127 0.0195 274.5525 0003315 321.0342 231.3211 1.00272249 49762Epoch: 2026-11-14T10:42Z
TLE epoch observation values (Epoch: 2026-11-14T10:42:29.193Z)
Latitude
-0.00449°
Longitude
-107.32373°
Altitude
35,794.74 km
Speed
3.074 km/s
True Right ascension
07h 07m 23s
True Declination
0° 00' 16"
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
14:00:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,801.513 km
Perigee altitude
35,773.557 km
Semi-major axis
42,165.672 km
Eccentricity
0.00033
Inclination
0.0195°
RAAN
274.5525°
Arg. of periapsis
321.0342°
True anomaly
231.29145°
Mean anomaly
231.3211°
Eccentric anomaly
231.30628°
Mean motion
0.25067 °/min
Orbital period
1,436.14 mins
BSTAR
0
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Other satellites on launch #14 in the year 2013 (2013-04-15 UTC)
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ANIK G1 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. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2026-11-14 17:25:42.941Z | 183.416° SSW | 2026-11-15 04:14:42.941Z | 183.35° SSW | 43.838° | 2026-11-15 17:25:42.941Z | 183.413° SSW |
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39127 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
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