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 26074.50984652 +.00000000 +00000-0 +46059-4 0 00000
2 22287 82.5275 347.4467 0022804 320.4470 39.5078 14.80057029 01
| Epoch (UTC): | 15 March 2026 12:14:10 |
| Eccentricity: | 0.0022804 |
| inclination: | 82.5275° |
| perigee height: | 613 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 347.4467° |
| argument of perigee: | 320.4470° |
| revolutions per day: | 14.80057029 |
| mean anomaly at epoch: | 39.5078° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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