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 21903U 26065.29154369 +.00000000 +00000-0 +75651-4 0 00004
2 21903 82.9415 344.7875 0041729 215.9351 258.0494 13.74743340 01
| Epoch (UTC): | 06 March 2026 06:59:49 |
| Eccentricity: | 0.0041729 |
| inclination: | 82.9415° |
| perigee height: | 952 km |
| apogee height: | 1013 km |
| right ascension of ascending node: | 344.7875° |
| argument of perigee: | 215.9351° |
| revolutions per day: | 13.74743340 |
| mean anomaly at epoch: | 258.0494° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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