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 22137.10607388 .00003885 00000-0 40481-3 0 9994
2 40025 97.9598 74.2682 0012800 153.2521 206.9359 14.90335768429600
| Epoch (UTC): | 17 May 2022 02:32:44 |
| Eccentricity: | 0.0012800 |
| inclination: | 97.9598° |
| perigee height: | 588 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 74.2682° |
| argument of perigee: | 153.2521° |
| revolutions per day: | 14.90335768 |
| mean anomaly at epoch: | 206.9359° |
| orbit number at epoch: | 42960 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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