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 25197.79149892 .00000009 00000-0 65668-4 0 9998
2 00116 66.8109 351.4611 0071987 153.1008 207.3833 13.92247285250018
| Epoch (UTC): | 16 July 2025 18:59:45 |
| Eccentricity: | 0.0071987 |
| inclination: | 66.8109° |
| perigee height: | 868 km |
| apogee height: | 973 km |
| right ascension of ascending node: | 351.4611° |
| argument of perigee: | 153.1008° |
| revolutions per day: | 13.92247285 |
| mean anomaly at epoch: | 207.3833° |
| orbit number at epoch: | 25001 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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