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 25397U 98043D 23334.82747544 .00000334 00000-0 16566-3 0 9993
2 25397 98.8939 293.9095 0001905 47.8742 312.2598 14.23950628319269
| Epoch (UTC): | 30 November 2023 19:51:33 |
| Eccentricity: | 0.0001905 |
| inclination: | 98.8939° |
| perigee height: | 810 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 293.9095° |
| argument of perigee: | 47.8742° |
| revolutions per day: | 14.23950628 |
| mean anomaly at epoch: | 312.2598° |
| orbit number at epoch: | 31926 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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