Showing default

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.

Loading next visibility...
Identifier
68490, 2026-067CC
Orbit
SSO
Country
Flag of NONO / NOR
Related business
Manufacturer
OHB-SE
Mission
Operational Commercial Communications
Bus & Motor
MIMIR, Unknown motor
Mass
93 kg wet, 93 kg dry
Launch date (UTC)
2026-03-30 (4 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan + 1 Ant, 1.6 m
Radar Cross Section
0.940 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago
0 MIMIR 1
1 68490U 26067CC  26217.47126011  .00001313  00000-0  13861-3 0  9998
2 68490  97.7644 174.8672 0001223 171.9363 188.1875 14.90948824 19062
Epoch: 2026-08-05T11:18Z
TLE epoch observation values (Epoch: 2026-08-05T11:18:36.873Z)
Latitude
-0.00004°
Longitude
51.18838°
Altitude
598.86 km
Speed
7.56 km/s
True Right ascension
11h 39m 28s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
19:01:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
592.848 km
Perigee altitude
591.143 km
Semi-major axis
6,970.133 km
Eccentricity
0.00012
Inclination
97.7644°
RAAN
174.8672°
Arg. of periapsis
171.9363°
True anomaly
188.1855°
Mean anomaly
188.1875°
Eccentric anomaly
188.1865°
Mean motion
3.72977 °/min
Orbital period
96.52 mins
BSTAR
0.00013861
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|