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 35685U 09041E 23083.52824525 .00004347 00000-0 49273-3 0 9996
2 35685 98.1273 158.0372 0058324 71.9925 288.7634 14.85685955738686
| Epoch (UTC): | 24 March 2023 12:40:40 |
| Eccentricity: | 0.0058324 |
| inclination: | 98.1273° |
| perigee height: | 570 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 158.0372° |
| argument of perigee: | 71.9925° |
| revolutions per day: | 14.85685955 |
| mean anomaly at epoch: | 288.7634° |
| orbit number at epoch: | 73868 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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