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 26129.54752280 +.00000000 +00000-0 -53066-4 0 00006
2 21903 82.9336 297.1627 0043455 39.5779 23.2489 13.74742548 06
| Epoch (UTC): | 09 May 2026 13:08:25 |
| Eccentricity: | 0.0043455 |
| inclination: | 82.9336° |
| perigee height: | 951 km |
| apogee height: | 1015 km |
| right ascension of ascending node: | 297.1627° |
| argument of perigee: | 39.5779° |
| revolutions per day: | 13.74742548 |
| mean anomaly at epoch: | 23.2489° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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