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 24278U 96046B 24281.06109518 .00000125 00000-0 16575-3 0 9990
2 24278 98.5810 201.0512 0348947 258.4735 97.7038 13.53215106389816
| Epoch (UTC): | 07 October 2024 01:27:58 |
| Eccentricity: | 0.0348947 |
| inclination: | 98.5810° |
| perigee height: | 801 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 201.0512° |
| argument of perigee: | 258.4735° |
| revolutions per day: | 13.53215106 |
| mean anomaly at epoch: | 97.7038° |
| orbit number at epoch: | 38981 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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