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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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, 1.2 m
Radar Cross Section
0.202 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 NORSAT 2
1 42828U 17042D 26034.42807071 .00015380 00000-0 74291-3 0 9995
2 42828 97.3928 210.3435 0010241 156.1713 203.9998 15.18689735467419Epoch: 2026-02-03T10:16Z
TLE epoch observation values (Epoch: 2026-02-03T10:16:25.309Z)
Latitude
0.00003°
Longitude
-77.37111°
Altitude
519.335 km
Speed
7.6 km/s
True Right ascension
14h 01m 22s
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
22:51:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
513.817 km
Perigee altitude
499.716 km
Semi-major axis
6,884.904 km
Eccentricity
0.00102
Inclination
97.3928°
RAAN
210.3435°
Arg. of periapsis
156.1713°
True anomaly
203.95212°
Mean anomaly
203.9998°
Eccentric anomaly
203.97596°
Mean motion
3.79924 °/min
Orbital period
94.76 mins
BSTAR
0.00074291
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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 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-03 23:30:33.173Z | 57.55° ENE | 2026-02-03 23:32:33.173Z | 91.461° ESE | 14.646° | 2026-02-03 23:34:33.173Z | 126.351° SE |
| 5 mins | 2026-02-04 01:04:33.173Z | 339.342° N | 2026-02-04 01:06:33.173Z | 291.297° WNW | 27.085° | 2026-02-04 01:09:33.173Z | 228.012° WSW |
| 6 mins | 2026-02-04 11:42:33.173Z | 170.401° S | 2026-02-04 11:45:33.173Z | 333.853° NNW | 42.199° | 2026-02-04 11:48:33.173Z | 346.51° N |
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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