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 25131.97144164 .00005556 00000-0 67411-3 0 9990
2 00107 28.7865 105.2425 0504804 348.5087 10.4328 14.19540501219382
| Epoch (UTC): | 11 May 2025 23:18:52 |
| Eccentricity: | 0.0504804 |
| inclination: | 28.7865° |
| perigee height: | 463 km |
| apogee height: | 1190 km |
| right ascension of ascending node: | 105.2425° |
| argument of perigee: | 348.5087° |
| revolutions per day: | 14.19540501 |
| mean anomaly at epoch: | 10.4328° |
| orbit number at epoch: | 21938 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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