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 16631U 86014H 25198.50681180 .00007386 00000-0 43002-3 0 9996
2 16631 63.2908 249.2024 0796809 105.9804 263.0440 13.84972731297873
| Epoch (UTC): | 17 July 2025 12:09:48 |
| Eccentricity: | 0.0796809 |
| inclination: | 63.2908° |
| perigee height: | 362 km |
| apogee height: | 1530 km |
| right ascension of ascending node: | 249.2024° |
| argument of perigee: | 105.9804° |
| revolutions per day: | 13.84972731 |
| mean anomaly at epoch: | 263.0440° |
| orbit number at epoch: | 29787 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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