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 00053U 60009E 24281.76983656 .00000035 00000-0 11860-2 0 9996
2 00053 47.2757 86.8154 0099764 51.8049 309.1674 12.17350747860210
| Epoch (UTC): | 07 October 2024 18:28:33 |
| Eccentricity: | 0.0099764 |
| inclination: | 47.2757° |
| perigee height: | 1524 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 86.8154° |
| argument of perigee: | 51.8049° |
| revolutions per day: | 12.17350747 |
| mean anomaly at epoch: | 309.1674° |
| orbit number at epoch: | 86021 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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