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 22888U 93070A 18142.40691965 +.00000051 +00000-0 +36812-4 0 9993
2 22888 082.9498 102.4190 0049169 131.0550 345.0046 13.74916497228938
| Epoch (UTC): | 22 May 2018 09:45:57 |
| Eccentricity: | 0.0049169 |
| inclination: | 82.9498° |
| perigee height: | 946 km |
| apogee height: | 1018 km |
| right ascension of ascending node: | 102.4190° |
| argument of perigee: | 131.0550° |
| revolutions per day: | 13.74916497 |
| mean anomaly at epoch: | 345.0046° |
| orbit number at epoch: | 22893 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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