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 40024U 14033Q 25073.53391953 .00026285 00000-0 14126-2 0 9995
2 40024 98.0895 65.6204 0004523 7.1968 352.9326 15.14866728584015
| Epoch (UTC): | 14 March 2025 12:48:50 |
| Eccentricity: | 0.0004523 |
| inclination: | 98.0895° |
| perigee height: | 518 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 65.6204° |
| argument of perigee: | 7.1968° |
| revolutions per day: | 15.14866728 |
| mean anomaly at epoch: | 352.9326° |
| orbit number at epoch: | 58401 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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