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 17720U 70025PJ 24358.03848663 .00009702 00000-0 47096-2 0 9997
2 17720 99.6356 196.0935 0034171 278.1623 234.4873 14.18219030 29253
| Epoch (UTC): | 23 December 2024 00:55:25 |
| Eccentricity: | 0.0034171 |
| inclination: | 99.6356° |
| perigee height: | 807 km |
| apogee height: | 856 km |
| right ascension of ascending node: | 196.0935° |
| argument of perigee: | 278.1623° |
| revolutions per day: | 14.18219030 |
| mean anomaly at epoch: | 234.4873° |
| orbit number at epoch: | 2925 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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