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 44612U 17060E 24357.49550628 .00007326 00000-0 80744-3 0 9995
2 44612 97.6016 10.4121 0013480 96.6329 263.6423 14.87732260386146
| Epoch (UTC): | 22 December 2024 11:53:31 |
| Eccentricity: | 0.0013480 |
| inclination: | 97.6016° |
| perigee height: | 595 km |
| apogee height: | 614 km |
| right ascension of ascending node: | 10.4121° |
| argument of perigee: | 96.6329° |
| revolutions per day: | 14.87732260 |
| mean anomaly at epoch: | 263.6423° |
| orbit number at epoch: | 38614 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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