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 22176.51442742 .00001970 00000-0 20725-3 0 9995
2 40025 97.9605 113.9762 0013233 36.9865 323.2262 14.90532693434965
| Epoch (UTC): | 25 June 2022 12:20:46 |
| Eccentricity: | 0.0013233 |
| inclination: | 97.9605° |
| perigee height: | 587 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 113.9762° |
| argument of perigee: | 36.9865° |
| revolutions per day: | 14.90532693 |
| mean anomaly at epoch: | 323.2262° |
| orbit number at epoch: | 43496 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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