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 21796U 26106.68201016 +.00000000 +00000-0 +32506-4 0 00007
2 21796 82.9579 216.3027 0049983 152.3477 321.1512 13.75758718 07
| Epoch (UTC): | 16 April 2026 16:22:05 |
| Eccentricity: | 0.0049983 |
| inclination: | 82.9579° |
| perigee height: | 942 km |
| apogee height: | 1016 km |
| right ascension of ascending node: | 216.3027° |
| argument of perigee: | 152.3477° |
| revolutions per day: | 13.75758718 |
| mean anomaly at epoch: | 321.1512° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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