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 22287U 26073.49574992 +.00000000 +00000-0 +60125-4 0 00009
2 22287 82.5275 348.3909 0022887 323.8926 36.0740 14.80056683 09
| Epoch (UTC): | 14 March 2026 11:53:52 |
| Eccentricity: | 0.0022887 |
| inclination: | 82.5275° |
| perigee height: | 613 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 348.3909° |
| argument of perigee: | 323.8926° |
| revolutions per day: | 14.80056683 |
| mean anomaly at epoch: | 36.0740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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