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 30514U 99025AJC 24358.02503299 .00003420 00000-0 10727-2 0 9998
2 30514 98.4480 24.4986 0179092 67.9916 294.0188 14.32391380931354
| Epoch (UTC): | 23 December 2024 00:36:02 |
| Eccentricity: | 0.0179092 |
| inclination: | 98.4480° |
| perigee height: | 655 km |
| apogee height: | 912 km |
| right ascension of ascending node: | 24.4986° |
| argument of perigee: | 67.9916° |
| revolutions per day: | 14.32391380 |
| mean anomaly at epoch: | 294.0188° |
| orbit number at epoch: | 93135 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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