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 00694U 63047A 24281.24904002 .00005192 00000-0 63908-3 0 9993
2 00694 30.3558 206.4902 0561272 201.4925 156.1210 14.08685653 58368
| Epoch (UTC): | 07 October 2024 05:58:37 |
| Eccentricity: | 0.0561272 |
| inclination: | 30.3558° |
| perigee height: | 457 km |
| apogee height: | 1270 km |
| right ascension of ascending node: | 206.4902° |
| argument of perigee: | 201.4925° |
| revolutions per day: | 14.08685653 |
| mean anomaly at epoch: | 156.1210° |
| orbit number at epoch: | 5836 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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