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 21797U 26106.24007127 +.00000000 +00000-0 +51480-4 0 00009
2 21797 82.9566 186.3690 0038904 51.9174 2.2820 13.77869974 03
| Epoch (UTC): | 16 April 2026 05:45:42 |
| Eccentricity: | 0.0038904 |
| inclination: | 82.9566° |
| perigee height: | 943 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 186.3690° |
| argument of perigee: | 51.9174° |
| revolutions per day: | 13.77869974 |
| mean anomaly at epoch: | 2.2820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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