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: 12 hours ago
TLE from 12 hours ago
0 NIMIQ 6
1 38342U 12026A 25354.47147500 -.00000150 00000-0 00000-0 0 9995
2 38342 0.0152 315.3075 0002462 307.6972 264.9354 1.00273217 48628Epoch: 2025-12-20T11:18Z
TLE epoch observation values (Epoch: 2025-12-20T11:18:55.439Z)
Latitude
-0.00949°
Longitude
-91.12676°
Altitude
35,786.621 km
Speed
3.075 km/s
True Right ascension
11h 11m 36s
True Declination
0° 00' 34"
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
22:15:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,797.645 km
Perigee altitude
35,776.883 km
Semi-major axis
42,165.401 km
Eccentricity
0.00025
Inclination
0.0152°
RAAN
315.3075°
Arg. of periapsis
307.6972°
True anomaly
264.9073°
Mean anomaly
264.9354°
Eccentric anomaly
264.92135°
Mean motion
0.25067 °/min
Orbital period
1,436.13 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 | 2025-12-20 23:16:40.454Z | 158.681° S | 2025-12-21 06:10:40.454Z | 158.716° S | 33.601° | 2025-12-21 23:16:40.454Z | 158.673° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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