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 23036.91293659 .00000078 00000-0 10869-3 0 9992
2 00016 34.2652 252.4400 2026697 340.4019 12.8461 10.48809963559998
| Epoch (UTC): | 05 February 2023 21:54:37 |
| Eccentricity: | 0.2026697 |
| inclination: | 34.2652° |
| perigee height: | 651 km |
| apogee height: | 4224 km |
| right ascension of ascending node: | 252.4400° |
| argument of perigee: | 340.4019° |
| revolutions per day: | 10.48809963 |
| mean anomaly at epoch: | 12.8461° |
| orbit number at epoch: | 55999 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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