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 Commercial Communications
Bus & Motor
MIMIR, Unknown motor
Mass
93 kg wet, 93 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan + 1 Ant, 1.1 m
Radar Cross Section
0.940 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 MIMIR 1
1 68490U 26067CC 26263.44157940 .00001339 00000-0 14075-3 0 9997
2 68490 97.7718 220.1189 0003646 79.1396 281.0233 14.91079388 25911Epoch: 2026-09-20T10:35Z
TLE epoch observation values (Epoch: 2026-09-20T10:35:52.460Z)
Latitude
0.00004°
Longitude
61.8146°
Altitude
597.124 km
Speed
7.561 km/s
True Right ascension
14h 40m 28s
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
12:54:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.13 km
Perigee altitude
589.048 km
Semi-major axis
6,969.726 km
Eccentricity
0.00036
Inclination
97.7718°
RAAN
220.1189°
Arg. of periapsis
79.1396°
True anomaly
280.98229°
Mean anomaly
281.0233°
Eccentric anomaly
281.00279°
Mean motion
3.73009 °/min
Orbital period
96.51 mins
BSTAR
0.00014075
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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 | 2026-09-20 20:23:56.644Z | 121.768° SE | 2026-09-20 20:26:56.644Z | 74.993° E | 23.843° | 2026-09-20 20:29:56.644Z | 20.955° NNE |
| 5 mins | 2026-09-20 22:00:56.644Z | 226.252° WSW | 2026-09-20 22:02:56.644Z | 270.176° WNW | 26.244° | 2026-09-20 22:05:56.644Z | 319.736° NNW |
| 6 mins | 2026-09-21 09:43:56.644Z | 34.042° NE | 2026-09-21 09:45:56.644Z | 76.654° E | 44.628° | 2026-09-21 09:49:56.644Z | 171.635° S |
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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