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 25166.70391274 .00001960 00000-0 22304-3 0 9992
2 00107 28.7908 265.7614 0504118 311.6229 44.2199 14.19796370224327
| Epoch (UTC): | 15 June 2025 16:53:38 |
| Eccentricity: | 0.0504118 |
| inclination: | 28.7908° |
| perigee height: | 463 km |
| apogee height: | 1189 km |
| right ascension of ascending node: | 265.7614° |
| argument of perigee: | 311.6229° |
| revolutions per day: | 14.19796370 |
| mean anomaly at epoch: | 44.2199° |
| orbit number at epoch: | 22432 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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