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 25167.96956328 .00001815 00000-0 20558-3 0 9996
2 107 28.7901 258.4909 0504079 323.4024 33.3095 14.19801044224055
| Epoch (UTC): | 16 June 2025 23:16:10 |
| Eccentricity: | 0.0504079 |
| inclination: | 28.7901° |
| perigee height: | 463 km |
| apogee height: | 1189 km |
| right ascension of ascending node: | 258.4909° |
| argument of perigee: | 323.4024° |
| revolutions per day: | 14.19801044 |
| mean anomaly at epoch: | 33.3095° |
| orbit number at epoch: | 22405 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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