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 30656U 99025APN 23033.28164054 .00005399 00000-0 24613-2 0 9990
2 30656 98.9804 157.3814 0048575 243.4052 116.2142 14.21407866821656
| Epoch (UTC): | 02 February 2023 06:45:33 |
| Eccentricity: | 0.0048575 |
| inclination: | 98.9804° |
| perigee height: | 785 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 157.3814° |
| argument of perigee: | 243.4052° |
| revolutions per day: | 14.21407866 |
| mean anomaly at epoch: | 116.2142° |
| orbit number at epoch: | 82165 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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