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 22178.46122645 .00001583 00000-0 16773-3 0 9996
2 40025 97.9609 115.9383 0013068 30.6251 329.5727 14.90538780435257
| Epoch (UTC): | 27 June 2022 11:04:09 |
| Eccentricity: | 0.0013068 |
| inclination: | 97.9609° |
| perigee height: | 587 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 115.9383° |
| argument of perigee: | 30.6251° |
| revolutions per day: | 14.90538780 |
| mean anomaly at epoch: | 329.5727° |
| orbit number at epoch: | 43525 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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