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: 10 hours ago
TLE from 10 hours ago
0 NORSAT 2
1 42828U 17042D 25289.13755184 .00012275 00000-0 65538-3 0 9995
2 42828 97.3915 102.7739 0010891 179.0644 181.0611 15.15215442450691Epoch: 2025-10-16T03:18Z
TLE epoch observation values (Epoch: 2025-10-16T03:18:04.478Z)
Latitude
-0.00004°
Longitude
28.35366°
Altitude
530.922 km
Speed
7.593 km/s
True Right ascension
06h 51m 05s
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
07:57:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
524.806 km
Perigee altitude
509.786 km
Semi-major axis
6,895.433 km
Eccentricity
0.00109
Inclination
97.3915°
RAAN
102.7739°
Arg. of periapsis
179.0644°
True anomaly
181.05879°
Mean anomaly
181.0611°
Eccentric anomaly
181.05995°
Mean motion
3.79054 °/min
Orbital period
94.97 mins
BSTAR
0.00065538
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-17 00:27:41.636Z | 15.28° NNE | 2025-10-17 00:31:41.636Z | 159.338° S | 42.257° | 2025-10-17 00:34:41.636Z | 187.635° SSW |
| 4 mins | 2025-10-17 11:09:41.636Z | 110.52° ESE | 2025-10-17 11:10:41.636Z | 84.973° E | 26.439° | 2025-10-17 11:13:41.636Z | 15.981° NNE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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