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 40025U 14033R 22179.80384287 .00001230 00000-0 13160-3 0 9993
2 40025 97.9609 117.2915 0012970 26.5879 333.6001 14.90541939435457
| Epoch (UTC): | 28 June 2022 19:17:32 |
| Eccentricity: | 0.0012970 |
| inclination: | 97.9609° |
| perigee height: | 587 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 117.2915° |
| argument of perigee: | 26.5879° |
| revolutions per day: | 14.90541939 |
| mean anomaly at epoch: | 333.6001° |
| orbit number at epoch: | 43545 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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