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 00016U 58002A 22279.24571306 -.00000052 00000-0 -84211-4 0 9991
2 00016 34.2640 246.7220 2027395 183.1694 175.3976 10.48816194547119
| Epoch (UTC): | 06 October 2022 05:53:49 |
| Eccentricity: | 0.2027395 |
| inclination: | 34.2640° |
| perigee height: | 650 km |
| apogee height: | 4225 km |
| right ascension of ascending node: | 246.7220° |
| argument of perigee: | 183.1694° |
| revolutions per day: | 10.48816194 |
| mean anomaly at epoch: | 175.3976° |
| orbit number at epoch: | 54711 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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