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: 11 hours ago
TLE from 11 hours ago
0 NORSAT 1
1 42826U 17042B 26119.42318597 .00006265 00000-0 35364-3 0 9997
2 42826 97.4403 288.2607 0005994 246.4576 113.6026 15.13473040479855Epoch: 2026-04-29T10:09Z
TLE epoch observation values (Epoch: 2026-04-29T10:09:23.267Z)
Latitude
-0.00005°
Longitude
-81.4706°
Altitude
530.358 km
Speed
7.597 km/s
True Right ascension
19h 13m 02s
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
04:40:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
526.73 km
Perigee altitude
518.458 km
Semi-major axis
6,900.731 km
Eccentricity
0.0006
Inclination
97.4403°
RAAN
288.2607°
Arg. of periapsis
246.4576°
True anomaly
113.66552°
Mean anomaly
113.6026°
Eccentric anomaly
113.63406°
Mean motion
3.78617 °/min
Orbital period
95.08 mins
BSTAR
0.00035364
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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 | 2026-04-29 23:25:52.105Z | 45.347° ENE | 2026-04-29 23:27:52.105Z | 83.846° E | 23.55° | 2026-04-29 23:30:52.105Z | 148.299° SSE |
| 4 mins | 2026-04-30 01:00:52.105Z | 321.742° NNW | 2026-04-30 01:02:52.105Z | 280.831° WNW | 18.166° | 2026-04-30 01:04:52.105Z | 247.463° WSW |
| 5 mins | 2026-04-30 11:40:52.105Z | 199.302° SSW | 2026-04-30 11:42:52.105Z | 250.923° W | 33.803° | 2026-04-30 11:45:52.105Z | 328.471° NNW |
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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