MIMIR 1, 68490
Orbit data source: Space-Track
MIMIR 1, 68490 is a Norwegian payload satellite 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
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 MIMIR 1
1 68490U 26067CC 26126.80507351 .00001693 00000-0 17503-3 0 9992
2 68490 97.7591 85.6920 0003155 132.2247 227.9240 14.91426065 5551Epoch: 2026-05-06T19:19Z
TLE epoch observation values (Epoch: 2026-05-06T19:19:18.351Z)
Latitude
0.00002°
Longitude
-68.79476°
Altitude
598.004 km
Speed
7.56 km/s
True Right ascension
05h 42m 46s
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
02:58:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
592.706 km
Perigee altitude
588.309 km
Semi-major axis
6,968.644 km
Eccentricity
0.00032
Inclination
97.7591°
RAAN
85.692°
Arg. of periapsis
132.2247°
True anomaly
227.89717°
Mean anomaly
227.924°
Eccentric anomaly
227.91059°
Mean motion
3.73096 °/min
Orbital period
96.49 mins
BSTAR
0.00017503
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-07 21:12:19.734Z | 164.063° S | 2026-05-07 21:16:19.734Z | 4.011° NNE | 43.501° | 2026-05-07 21:19:19.734Z | 349.297° N |
| 6 mins | 2026-05-08 10:32:19.734Z | 352.995° N | 2026-05-08 10:35:19.734Z | 275.655° WNW | 35.316° | 2026-05-08 10:38:19.734Z | 217.572° SW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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