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 25133.16704133 .00005320 00000-0 64502-3 0 9998
2 107 28.7862 98.3765 0504767 359.6321 0.3845 14.19552338219103
| Epoch (UTC): | 13 May 2025 04:00:32 |
| Eccentricity: | 0.0504767 |
| inclination: | 28.7862° |
| perigee height: | 463 km |
| apogee height: | 1190 km |
| right ascension of ascending node: | 98.3765° |
| argument of perigee: | 359.6321° |
| revolutions per day: | 14.19552338 |
| mean anomaly at epoch: | 0.3845° |
| orbit number at epoch: | 21910 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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