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 25682U 99020A 23154.71622958 .00000477 00000-0 10835-3 0 9996
2 25682 97.9298 193.6260 0001823 93.8660 18.2065 14.60104804283814
| Epoch (UTC): | 03 June 2023 17:11:22 |
| Eccentricity: | 0.0001823 |
| inclination: | 97.9298° |
| perigee height: | 691 km |
| apogee height: | 694 km |
| right ascension of ascending node: | 193.6260° |
| argument of perigee: | 93.8660° |
| revolutions per day: | 14.60104804 |
| mean anomaly at epoch: | 18.2065° |
| orbit number at epoch: | 28381 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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