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 00107U 61013A 24277.74998160 .00006617 00000-0 82599-3 0 9991
2 00107 28.7848 287.2606 0515484 104.4844 261.3467 14.16824236188092
| Epoch (UTC): | 03 October 2024 17:59:58 |
| Eccentricity: | 0.0515484 |
| inclination: | 28.7848° |
| perigee height: | 464 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 287.2606° |
| argument of perigee: | 104.4844° |
| revolutions per day: | 14.16824236 |
| mean anomaly at epoch: | 261.3467° |
| orbit number at epoch: | 18809 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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