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 23265.47903921 .00000505 00000-0 68867-3 0 9993
2 00016 34.2725 312.4063 2020596 224.3071 117.7080 10.48891243583992
| Epoch (UTC): | 22 September 2023 11:29:48 |
| Eccentricity: | 0.2020596 |
| inclination: | 34.2725° |
| perigee height: | 656 km |
| apogee height: | 4218 km |
| right ascension of ascending node: | 312.4063° |
| argument of perigee: | 224.3071° |
| revolutions per day: | 10.48891243 |
| mean anomaly at epoch: | 117.7080° |
| orbit number at epoch: | 58399 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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