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 25339.31406455 .00002966 00000-0 34771-3 0 9997
2 00107 28.7830 353.4270 0498856 118.9009 246.2537 14.20980605248884
| Epoch (UTC): | 05 December 2025 07:32:15 |
| Eccentricity: | 0.0498856 |
| inclination: | 28.7830° |
| perigee height: | 463 km |
| apogee height: | 1181 km |
| right ascension of ascending node: | 353.4270° |
| argument of perigee: | 118.9009° |
| revolutions per day: | 14.20980605 |
| mean anomaly at epoch: | 246.2537° |
| orbit number at epoch: | 24888 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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