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 data is extracted from the following two-line orbital elements,
1 22287U 92094B 22146.50910147 .00000331 00000-0 42274-4 0 9997
2 22287 82.5255 199.0406 0024533 182.4487 177.6609 14.78282149564063
| Epoch (UTC): | 26 May 2022 12:13:06 |
| Eccentricity: | 0.0024533 |
| inclination: | 82.5255° |
| perigee height: | 617 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 199.0406° |
| argument of perigee: | 182.4487° |
| revolutions per day: | 14.78282149 |
| mean anomaly at epoch: | 177.6609° |
| orbit number at epoch: | 56406 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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