NIMIQ 6, 38342
Orbit data source: Space-Track
NIMIQ 6, 38342 is a payload satellite owned by Telesat (Loral) (CA) in GEO that was launched on Thu, 17 May 2012 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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38342 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CARelated business
Manufacturer
SS/Loral
Mission
Operational Commercial Communications
Bus & Motor
SSL-1300, R-4D
Mass
4,745 kg wet, ~2,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 13.0 m
Radar Cross Section
34.256 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 NIMIQ 6
1 38342U 12026A 25309.28267701 -.00000162 00000-0 00000-0 0 9993
2 38342 0.0406 71.6465 0003087 156.2299 187.5822 1.00271489 48167Epoch: 2025-11-05T06:47Z
TLE epoch observation values (Epoch: 2025-11-05T06:47:03.293Z)
Latitude
0.00998°
Longitude
-91.10593°
Altitude
35,799.137 km
Speed
3.074 km/s
True Right ascension
03h 41m 39s
True Declination
0° 00' 36"
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
12:25:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,800.765 km
Perigee altitude
35,774.732 km
Semi-major axis
42,165.885 km
Eccentricity
0.00031
Inclination
0.0406°
RAAN
71.6465°
Arg. of periapsis
156.2299°
True anomaly
187.57753°
Mean anomaly
187.5822°
Eccentric anomaly
187.57987°
Mean motion
0.25067 °/min
Orbital period
1,436.15 mins
BSTAR
0
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Other satellites on launch #26 in the year 2012 (2012-05-17 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.NIMIQ 6 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 | 2025-11-05 16:25:14.341Z | 158.763° S | 2025-11-06 08:16:14.341Z | 158.752° S | 33.596° | 2025-11-06 16:25:14.341Z | 158.761° S |
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38342 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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