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 30167U 99025TY 24279.90300138 .00008126 00000-0 20045-2 0 9990
2 30167 99.0124 332.2810 0149395 8.7367 164.8134 14.45847117930972
| Epoch (UTC): | 05 October 2024 21:40:19 |
| Eccentricity: | 0.0149395 |
| inclination: | 99.0124° |
| perigee height: | 633 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 332.2810° |
| argument of perigee: | 8.7367° |
| revolutions per day: | 14.45847117 |
| mean anomaly at epoch: | 164.8134° |
| orbit number at epoch: | 93097 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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