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 25861U 99039B 23153.10743346 .00000604 00000-0 88433-4 0 9994
2 25861 98.1389 190.2374 0014068 289.5444 70.4247 14.79329440287311
| Epoch (UTC): | 02 June 2023 02:34:42 |
| Eccentricity: | 0.0014068 |
| inclination: | 98.1389° |
| perigee height: | 621 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 190.2374° |
| argument of perigee: | 289.5444° |
| revolutions per day: | 14.79329440 |
| mean anomaly at epoch: | 70.4247° |
| orbit number at epoch: | 28731 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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