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 26064.23364073 +.00000000 +00000-0 +84413-4 0 00004
2 22287 82.5275 357.0133 0023696 354.9185 5.1784 14.80046640 03
| Epoch (UTC): | 05 March 2026 05:36:26 |
| Eccentricity: | 0.0023696 |
| inclination: | 82.5275° |
| perigee height: | 613 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 357.0133° |
| argument of perigee: | 354.9185° |
| revolutions per day: | 14.80046640 |
| mean anomaly at epoch: | 5.1784° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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