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 26072.27883370 +.00000000 +00000-0 +61489-4 0 00001
2 22287 82.5276 349.5237 0023007 328.0032 31.9783 14.80055408 02
| Epoch (UTC): | 13 March 2026 06:41:31 |
| Eccentricity: | 0.0023007 |
| inclination: | 82.5276° |
| perigee height: | 613 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 349.5237° |
| argument of perigee: | 328.0032° |
| revolutions per day: | 14.80055408 |
| mean anomaly at epoch: | 31.9783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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