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 14551U 83122A 24287.52372312 .00044203 00000-0 91910-3 0 9996
2 14551 82.4915 28.3637 0004070 303.9056 56.1805 15.45447474976645
| Epoch (UTC): | 13 October 2024 12:34:09 |
| Eccentricity: | 0.0004070 |
| inclination: | 82.4915° |
| perigee height: | 427 km |
| apogee height: | 433 km |
| right ascension of ascending node: | 28.3637° |
| argument of perigee: | 303.9056° |
| revolutions per day: | 15.45447474 |
| mean anomaly at epoch: | 56.1805° |
| orbit number at epoch: | 97664 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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