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 26076.20000659 +.00000000 +00000-0 +44808-4 0 00005
2 22287 82.5274 345.8732 0022682 314.6422 45.2941 14.80058400 00
| Epoch (UTC): | 17 March 2026 04:48:00 |
| Eccentricity: | 0.0022682 |
| inclination: | 82.5274° |
| perigee height: | 613 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 345.8732° |
| argument of perigee: | 314.6422° |
| revolutions per day: | 14.80058400 |
| mean anomaly at epoch: | 45.2941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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