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 21799U 26103.97762720 +.00000000 +00000-0 +40381-3 0 00002
2 21799 63.2963 316.5991 0883855 71.9974 297.5292 13.60920447 09
| Epoch (UTC): | 13 April 2026 23:27:46 |
| Eccentricity: | 0.0883855 |
| inclination: | 63.2963° |
| perigee height: | 377 km |
| apogee height: | 1687 km |
| right ascension of ascending node: | 316.5991° |
| argument of perigee: | 71.9974° |
| revolutions per day: | 13.60920447 |
| mean anomaly at epoch: | 297.5292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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