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 22142.65088872 .00000398 00000-0 51382-4 0 9993
2 22287 82.5261 202.6223 0024251 195.1725 164.8763 14.78279809563495
| Epoch (UTC): | 22 May 2022 15:37:16 |
| Eccentricity: | 0.0024251 |
| inclination: | 82.5261° |
| perigee height: | 618 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 202.6223° |
| argument of perigee: | 195.1725° |
| revolutions per day: | 14.78279809 |
| mean anomaly at epoch: | 164.8763° |
| orbit number at epoch: | 56349 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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