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 25399U 98043F 23274.12481709 .00000258 00000-0 12987-3 0 9997
2 25399 98.8428 229.1178 0002845 89.1836 270.9669 14.24957440311322
| Epoch (UTC): | 01 October 2023 02:59:44 |
| Eccentricity: | 0.0002845 |
| inclination: | 98.8428° |
| perigee height: | 806 km |
| apogee height: | 810 km |
| right ascension of ascending node: | 229.1178° |
| argument of perigee: | 89.1836° |
| revolutions per day: | 14.24957440 |
| mean anomaly at epoch: | 270.9669° |
| orbit number at epoch: | 31132 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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