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 25199.16497434 .00009065 00000-0 39463-3 0 9992
2 25979 98.1989 254.0234 0005829 163.0576 197.0854 15.22481236392923
| Epoch (UTC): | 18 July 2025 03:57:33 |
| Eccentricity: | 0.0005829 |
| inclination: | 98.1989° |
| perigee height: | 494 km |
| apogee height: | 502 km |
| right ascension of ascending node: | 254.0234° |
| argument of perigee: | 163.0576° |
| revolutions per day: | 15.22481236 |
| mean anomaly at epoch: | 197.0854° |
| orbit number at epoch: | 39292 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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