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 22179.53531984 .00001316 00000-0 14037-3 0 9990
2 40025 97.9609 117.0209 0012989 27.4150 332.7750 14.90541429435414
| Epoch (UTC): | 28 June 2022 12:50:51 |
| Eccentricity: | 0.0012989 |
| inclination: | 97.9609° |
| perigee height: | 587 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 117.0209° |
| argument of perigee: | 27.4150° |
| revolutions per day: | 14.90541429 |
| mean anomaly at epoch: | 332.7750° |
| orbit number at epoch: | 43541 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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