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 26065.51817061 +.00000000 +00000-0 +83247-4 0 00000
2 22287 82.5275 355.8174 0023575 350.6487 9.4284 14.80048139 05
| Epoch (UTC): | 06 March 2026 12:26:09 |
| Eccentricity: | 0.0023575 |
| inclination: | 82.5275° |
| perigee height: | 613 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 355.8174° |
| argument of perigee: | 350.6487° |
| revolutions per day: | 14.80048139 |
| mean anomaly at epoch: | 9.4284° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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