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 01504U 65065A 22331.28909194 .00000176 00000-0 30544-3 0 9998
2 01504 89.8918 251.1085 0066106 306.7558 224.1434 13.39676321793886
| Epoch (UTC): | 27 November 2022 06:56:17 |
| Eccentricity: | 0.0066106 |
| inclination: | 89.8918° |
| perigee height: | 1061 km |
| apogee height: | 1160 km |
| right ascension of ascending node: | 251.1085° |
| argument of perigee: | 306.7558° |
| revolutions per day: | 13.39676321 |
| mean anomaly at epoch: | 224.1434° |
| orbit number at epoch: | 79388 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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