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 05015U 71015J 24357.62462884 .00012153 00000-0 34884-2 0 9997
2 05015 65.7056 116.1536 0660422 217.3000 138.0431 13.62263569590858
| Epoch (UTC): | 22 December 2024 14:59:27 |
| Eccentricity: | 0.0660422 |
| inclination: | 65.7056° |
| perigee height: | 538 km |
| apogee height: | 1516 km |
| right ascension of ascending node: | 116.1536° |
| argument of perigee: | 217.3000° |
| revolutions per day: | 13.62263569 |
| mean anomaly at epoch: | 138.0431° |
| orbit number at epoch: | 59085 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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