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 09662U 77002B 25346.15447959 .00000056 00000-0 28240-4 0 9994
2 09662 81.2753 351.4841 0053041 62.4049 298.2489 14.01281244500436
| Epoch (UTC): | 12 December 2025 03:42:27 |
| Eccentricity: | 0.0053041 |
| inclination: | 81.2753° |
| perigee height: | 851 km |
| apogee height: | 928 km |
| right ascension of ascending node: | 351.4841° |
| argument of perigee: | 62.4049° |
| revolutions per day: | 14.01281244 |
| mean anomaly at epoch: | 298.2489° |
| orbit number at epoch: | 50043 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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