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 26104.07581373 +.00000000 +00000-0 +25422-4 0 00004
2 21796 82.9577 218.2314 0049823 159.5375 13.4547 13.75758556 03
| Epoch (UTC): | 14 April 2026 01:49:10 |
| Eccentricity: | 0.0049823 |
| inclination: | 82.9577° |
| perigee height: | 942 km |
| apogee height: | 1016 km |
| right ascension of ascending node: | 218.2314° |
| argument of perigee: | 159.5375° |
| revolutions per day: | 13.75758556 |
| mean anomaly at epoch: | 13.4547° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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