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 00058U 60013A 22331.77635501 .00000108 00000-0 31023-4 0 9990
2 00058 28.3279 242.5301 0164987 265.1971 92.9716 13.46340860 59080
| Epoch (UTC): | 27 November 2022 18:37:57 |
| Eccentricity: | 0.0164987 |
| inclination: | 28.3279° |
| perigee height: | 962 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 242.5301° |
| argument of perigee: | 265.1971° |
| revolutions per day: | 13.46340860 |
| mean anomaly at epoch: | 92.9716° |
| orbit number at epoch: | 5908 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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