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 15495U 85009B 24278.86079239 .00002845 00000-0 32782-3 0 9997
2 15495 82.5264 208.2936 0020007 163.2860 196.9020 14.85240938124310
| Epoch (UTC): | 04 October 2024 20:39:32 |
| Eccentricity: | 0.0020007 |
| inclination: | 82.5264° |
| perigee height: | 599 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 208.2936° |
| argument of perigee: | 163.2860° |
| revolutions per day: | 14.85240938 |
| mean anomaly at epoch: | 196.9020° |
| orbit number at epoch: | 12431 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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