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 25860U 99039A 23154.13681254 .00000824 00000-0 12284-3 0 9990
2 25860 98.0895 201.1444 0001537 72.5129 287.6249 14.77506843285020
| Epoch (UTC): | 03 June 2023 03:17:00 |
| Eccentricity: | 0.0001537 |
| inclination: | 98.0895° |
| perigee height: | 636 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 201.1444° |
| argument of perigee: | 72.5129° |
| revolutions per day: | 14.77506843 |
| mean anomaly at epoch: | 287.6249° |
| orbit number at epoch: | 28502 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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