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 25339.38430448 .00003012 00000-0 35342-3 0 9991
2 00107 28.7829 353.0230 0498860 119.5531 245.5712 14.20981189248892
| Epoch (UTC): | 05 December 2025 09:13:23 |
| Eccentricity: | 0.0498860 |
| inclination: | 28.7829° |
| perigee height: | 463 km |
| apogee height: | 1181 km |
| right ascension of ascending node: | 353.0230° |
| argument of perigee: | 119.5531° |
| revolutions per day: | 14.20981189 |
| mean anomaly at epoch: | 245.5712° |
| orbit number at epoch: | 24889 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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