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 25979U 99064C 25191.60644209 .00005770 00000-0 25356-3 0 9992
2 25979 98.1996 245.7817 0005224 185.9788 174.1384 15.22353076391756
| Epoch (UTC): | 10 July 2025 14:33:16 |
| Eccentricity: | 0.0005224 |
| inclination: | 98.1996° |
| perigee height: | 495 km |
| apogee height: | 502 km |
| right ascension of ascending node: | 245.7817° |
| argument of perigee: | 185.9788° |
| revolutions per day: | 15.22353076 |
| mean anomaly at epoch: | 174.1384° |
| orbit number at epoch: | 39175 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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