MIMIR 1, 68490
Orbit data source: Space-Track
MIMIR 1, 68490 is a payload satellite owned by Space Norway (NO) in SSO that was launched on Mon, 30 Mar 2026 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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68490 intel report (Beta)
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Identifier
Orbit
Country
NO / NORRelated business
Manufacturer
OHB-SE
Mission
Operational spacecraft
Bus & Motor
MIMIR, Unknown motor
Mass
93 kg wet, 93 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 1.6 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 MIMIR 1
1 68490U 26067CC 26171.43024082 .00001740 00000-0 18165-3 0 9994
2 68490 97.7613 129.5837 0003313 49.6186 310.5322 14.90995453 12201Epoch: 2026-06-20T10:19Z
TLE epoch observation values (Epoch: 2026-06-20T10:19:32.806Z)
Latitude
0.00004°
Longitude
66.05202°
Altitude
596.37 km
Speed
7.562 km/s
True Right ascension
08h 38m 20s
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
10:53:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.159 km
Perigee altitude
589.541 km
Semi-major axis
6,969.987 km
Eccentricity
0.00033
Inclination
97.7613°
RAAN
129.5837°
Arg. of periapsis
49.6186°
True anomaly
310.50334°
Mean anomaly
310.5322°
Eccentric anomaly
310.51777°
Mean motion
3.72988 °/min
Orbital period
96.52 mins
BSTAR
0.00018165
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Other satellites on launch #67 in the year 2026 (2026-03-30 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.MIMIR 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-22 09:36:51.792Z | 35.132° NE | 2026-06-22 09:39:51.792Z | 100.248° ESE | 31.864° | 2026-06-22 09:42:51.792Z | 162.121° S |
| 5 mins | 2026-06-22 20:27:51.792Z | 112.24° ESE | 2026-06-22 20:29:51.792Z | 74.123° E | 22.962° | 2026-06-22 20:32:51.792Z | 19.36° NNE |
| 5 mins | 2026-06-22 22:03:51.792Z | 228.42° WSW | 2026-06-22 22:05:51.792Z | 270.908° WNW | 22.589° | 2026-06-22 22:08:51.792Z | 319.013° 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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