NORSAT 1, 42826
Orbit data source: Space-Track
NORSAT 1, 42826 is a payload satellite owned by Statsat (NO) in SSO that was launched on Fri, 14 Jul 2017 UTC via a SOYUZ-2-1A 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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42826 intel report (Beta)
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Identifier
Orbit
Country
NO / NORRelated business
Manufacturer
UTIAS-SFL
Mission
Operational Commercial Communications
Bus & Motor
GNB, Unknown motor
Mass
30 kg wet, 30 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan + 4 Ant, 1.0 m
Radar Cross Section
0.202 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 NORSAT 1
1 42826U 17042B 26168.53721767 .00005441 00000-0 30227-3 0 9998
2 42826 97.4448 336.2447 0008468 84.8855 275.3343 15.14084988487287Epoch: 2026-06-17T12:53Z
TLE epoch observation values (Epoch: 2026-06-17T12:53:35.606Z)
Latitude
-0.00005°
Longitude
-122.94713°
Altitude
526.301 km
Speed
7.6 km/s
True Right ascension
22h 24m 58s
True Declination
0° 00' 00"
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
08:33:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
526.575 km
Perigee altitude
514.891 km
Semi-major axis
6,898.87 km
Eccentricity
0.00085
Inclination
97.4448°
RAAN
336.2447°
Arg. of periapsis
84.8855°
True anomaly
275.23767°
Mean anomaly
275.3343°
Eccentric anomaly
275.28599°
Mean motion
3.78771 °/min
Orbital period
95.04 mins
BSTAR
0.00030227
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Other satellites on launch #42 in the year 2017 (2017-07-14 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.NORSAT 1 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-18 00:34:22.207Z | 339.86° N | 2026-06-18 00:36:22.207Z | 281.649° WNW | 30.909° | 2026-06-18 00:39:22.207Z | 221.594° SW |
| 5 mins | 2026-06-18 11:14:22.207Z | 166.184° S | 2026-06-18 11:16:22.207Z | 157.665° S | 44.597° | 2026-06-18 11:19:22.207Z | 348.472° N |
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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