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 22177.11860654 .00002042 00000-0 21458-3 0 9993
2 40025 97.9609 114.5852 0013162 34.7449 325.4625 14.90535515435561
| Epoch (UTC): | 26 June 2022 02:50:47 |
| Eccentricity: | 0.0013162 |
| inclination: | 97.9609° |
| perigee height: | 587 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 114.5852° |
| argument of perigee: | 34.7449° |
| revolutions per day: | 14.90535515 |
| mean anomaly at epoch: | 325.4625° |
| orbit number at epoch: | 43556 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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