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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Edit Public Description
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: 18 hours ago
TLE from 18 hours ago
0 NORSAT 1
1 42826U 17042B 26023.70788158 .00011202 00000-0 65791-3 0 9990
2 42826 97.4283 194.9688 0006574 217.7228 142.3543 15.11856988465383Epoch: 2026-01-23T16:59Z
TLE epoch observation values (Epoch: 2026-01-23T16:59:20.968Z)
Latitude
0.00003°
Longitude
177.08861°
Altitude
537.214 km
Speed
7.592 km/s
True Right ascension
12h 59m 52s
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
12:39:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
532.054 km
Perigee altitude
522.975 km
Semi-major axis
6,905.652 km
Eccentricity
0.00066
Inclination
97.4283°
RAAN
194.9688°
Arg. of periapsis
217.7228°
True anomaly
142.40028°
Mean anomaly
142.3543°
Eccentric anomaly
142.37729°
Mean motion
3.78213 °/min
Orbital period
95.18 mins
BSTAR
0.00065791
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Other satellites on launch #42 in the year 2017 (2017-07-14 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.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 | 2026-01-24 12:10:27.940Z | 216.138° SW | 2026-01-24 12:13:27.940Z | 268.997° W | 19.606° | 2026-01-24 12:15:27.940Z | 306.492° NW |
| 5 mins | 2026-01-24 23:45:27.940Z | 41.739° NE | 2026-01-24 23:47:27.940Z | 101.824° ESE | 33.032° | 2026-01-24 23:50:27.940Z | 166.559° S |
| 4 mins | 2026-01-25 10:27:27.940Z | 95.02° ESE | 2026-01-25 10:28:27.940Z | 75.298° E | 18.28° | 2026-01-25 10:31:27.940Z | 22.974° NE |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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