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 107U 61013A 24250.83289795 .00007056 00000-0 88110-3 0 9992
2 107 28.7880 81.1298 0516350 215.2337 141.3037 14.16546484183829
| Epoch (UTC): | 06 September 2024 19:59:22 |
| Eccentricity: | 0.0516350 |
| inclination: | 28.7880° |
| perigee height: | 464 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 81.1298° |
| argument of perigee: | 215.2337° |
| revolutions per day: | 14.16546484 |
| mean anomaly at epoch: | 141.3037° |
| orbit number at epoch: | 18382 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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