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 22825U 93061C 23157.36506403 .00000139 00000-0 71080-4 0 9996
2 22825 98.8414 200.0807 0009592 99.0246 261.2021 14.30305687548746
| Epoch (UTC): | 06 June 2023 08:45:41 |
| Eccentricity: | 0.0009592 |
| inclination: | 98.8414° |
| perigee height: | 784 km |
| apogee height: | 797 km |
| right ascension of ascending node: | 200.0807° |
| argument of perigee: | 99.0246° |
| revolutions per day: | 14.30305687 |
| mean anomaly at epoch: | 261.2021° |
| orbit number at epoch: | 54874 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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