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 30994U 99025BCL 24358.00504027 .00000474 00000-0 28460-3 0 9998
2 30994 98.7114 10.9639 0018837 105.2126 255.1131 14.11463158915961
| Epoch (UTC): | 23 December 2024 00:07:15 |
| Eccentricity: | 0.0018837 |
| inclination: | 98.7114° |
| perigee height: | 841 km |
| apogee height: | 868 km |
| right ascension of ascending node: | 10.9639° |
| argument of perigee: | 105.2126° |
| revolutions per day: | 14.11463158 |
| mean anomaly at epoch: | 255.1131° |
| orbit number at epoch: | 91596 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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