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 44616U 18031K 24355.46099415 .00007093 00000-0 75469-3 0 9994
2 44616 97.8400 72.7345 0004726 299.3350 60.7394 14.89250776345076
| Epoch (UTC): | 20 December 2024 11:03:49 |
| Eccentricity: | 0.0004726 |
| inclination: | 97.8400° |
| perigee height: | 597 km |
| apogee height: | 603 km |
| right ascension of ascending node: | 72.7345° |
| argument of perigee: | 299.3350° |
| revolutions per day: | 14.89250776 |
| mean anomaly at epoch: | 60.7394° |
| orbit number at epoch: | 34507 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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