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 23032.50901371 .00004641 00000-0 38163-3 0 9995
2 25979 98.2376 10.7482 0007092 1.8998 358.2249 14.99665689257509
| Epoch (UTC): | 01 February 2023 12:12:58 |
| Eccentricity: | 0.0007092 |
| inclination: | 98.2376° |
| perigee height: | 563 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 10.7482° |
| argument of perigee: | 1.8998° |
| revolutions per day: | 14.99665689 |
| mean anomaly at epoch: | 358.2249° |
| orbit number at epoch: | 25750 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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