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 22078U 92052C 23272.18532511 -.00000045 00000-0 67997-4 0 9991
2 22078 66.0849 187.5160 0008686 337.6886 22.3753 12.86814534462591
| Epoch (UTC): | 29 September 2023 04:26:52 |
| Eccentricity: | 0.0008686 |
| inclination: | 66.0849° |
| perigee height: | 1307 km |
| apogee height: | 1321 km |
| right ascension of ascending node: | 187.5160° |
| argument of perigee: | 337.6886° |
| revolutions per day: | 12.86814534 |
| mean anomaly at epoch: | 22.3753° |
| orbit number at epoch: | 46259 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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