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 26064.50327046 +.00000000 +00000-0 +71215-4 0 00003
2 21903 82.9415 345.3713 0041683 218.1725 316.7863 13.74743212 08
| Epoch (UTC): | 05 March 2026 12:04:42 |
| Eccentricity: | 0.0041683 |
| inclination: | 82.9415° |
| perigee height: | 952 km |
| apogee height: | 1013 km |
| right ascension of ascending node: | 345.3713° |
| argument of perigee: | 218.1725° |
| revolutions per day: | 13.74743212 |
| mean anomaly at epoch: | 316.7863° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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