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 00116U 61015A 25347.28102324 .00000077 00000-0 11705-3 0 9995
2 00116 66.8103 345.7209 0070734 39.4575 321.1625 13.92288538270826
| Epoch (UTC): | 13 December 2025 06:44:40 |
| Eccentricity: | 0.0070734 |
| inclination: | 66.8103° |
| perigee height: | 869 km |
| apogee height: | 972 km |
| right ascension of ascending node: | 345.7209° |
| argument of perigee: | 39.4575° |
| revolutions per day: | 13.92288538 |
| mean anomaly at epoch: | 321.1625° |
| orbit number at epoch: | 27082 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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