View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 44903U 26145.52753177 +.00000000 +00000-0 +00000-0 0 00008
2 44903 0.2006 80.4983 0001088 325.2174 103.2376 1.00271118 06
| Epoch (UTC): | 25 May 2026 12:39:38 |
| Eccentricity: | 0.0001088 |
| inclination: | 0.2006° |
| perigee height: | 35782 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 80.4983° |
| argument of perigee: | 325.2174° |
| revolutions per day: | 1.00271118 |
| mean anomaly at epoch: | 103.2376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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