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 42400U 00055SU 22183.61415653 .00000957 00000-0 53650-3 0 9990
2 42400 98.7279 239.7297 0023614 232.3182 127.5849 14.12848562321654
| Epoch (UTC): | 02 July 2022 14:44:23 |
| Eccentricity: | 0.0023614 |
| inclination: | 98.7279° |
| perigee height: | 832 km |
| apogee height: | 867 km |
| right ascension of ascending node: | 239.7297° |
| argument of perigee: | 232.3182° |
| revolutions per day: | 14.12848562 |
| mean anomaly at epoch: | 127.5849° |
| orbit number at epoch: | 32165 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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