NORSAT 2, 42828
Orbit data source: Space-Track
NORSAT 2, 42828 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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42828 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, 1.2 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 2
1 42828U 17042D 26134.29055931 .00007892 00000-0 35618-3 0 9990
2 42828 97.4019 308.2921 0010258 163.6256 196.5313 15.21216181482589Epoch: 2026-05-14T06:58Z
TLE epoch observation values (Epoch: 2026-05-14T06:58:24.324Z)
Latitude
-0.00003°
Longitude
-28.34759°
Altitude
512.031 km
Speed
7.604 km/s
True Right ascension
20h 33m 10s
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
09:30:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.19 km
Perigee altitude
492.08 km
Semi-major axis
6,877.272 km
Eccentricity
0.00103
Inclination
97.4019°
RAAN
308.2921°
Arg. of periapsis
163.6256°
True anomaly
196.49789°
Mean anomaly
196.5313°
Eccentric anomaly
196.51459°
Mean motion
3.80556 °/min
Orbital period
94.6 mins
BSTAR
0.00035618
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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 2 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-15 11:31:12.905Z | 159.672° S | 2026-05-15 11:34:12.905Z | 49.83° ENE | 43.533° | 2026-05-15 11:37:12.905Z | 352.738° N |
| 6 mins | 2026-05-16 00:35:12.905Z | 5.231° NNE | 2026-05-16 00:38:12.905Z | 233.797° WSW | 41.449° | 2026-05-16 00:41:12.905Z | 200.109° SSW |
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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