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 25196.50522412 -.00000045 00000-0 65663-4 0 9991
2 22078 66.0838 254.0883 0001538 63.2945 296.8230 12.86843090546914
| Epoch (UTC): | 15 July 2025 12:07:31 |
| Eccentricity: | 0.0001538 |
| inclination: | 66.0838° |
| perigee height: | 1313 km |
| apogee height: | 1315 km |
| right ascension of ascending node: | 254.0883° |
| argument of perigee: | 63.2945° |
| revolutions per day: | 12.86843090 |
| mean anomaly at epoch: | 296.8230° |
| orbit number at epoch: | 54691 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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