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 22921U 26150.34563146 +.00000000 +00000-0 +00000-0 0 00005
2 22921 12.9432 1.2330 0002072 43.5801 246.1987 0.98517566 04
| Epoch (UTC): | 30 May 2026 08:17:42 |
| Eccentricity: | 0.0002072 |
| inclination: | 12.9432° |
| perigee height: | 36277 km |
| apogee height: | 36294 km |
| right ascension of ascending node: | 1.2330° |
| argument of perigee: | 43.5801° |
| revolutions per day: | 0.98517566 |
| mean anomaly at epoch: | 246.1987° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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