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 23151.55173417 .00000557 00000-0 82040-4 0 9992
2 25861 98.1391 188.6623 0014110 295.0352 64.9394 14.79327209286951
| Epoch (UTC): | 31 May 2023 13:14:29 |
| Eccentricity: | 0.0014110 |
| inclination: | 98.1391° |
| perigee height: | 621 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 188.6623° |
| argument of perigee: | 295.0352° |
| revolutions per day: | 14.79327209 |
| mean anomaly at epoch: | 64.9394° |
| orbit number at epoch: | 28695 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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