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 22181.59964566 .00000075 00000-0 11944-3 0 9990
2 01504 89.8828 252.8198 0066607 12.3731 112.3857 13.39625596773847
| Epoch (UTC): | 30 June 2022 14:23:29 |
| Eccentricity: | 0.0066607 |
| inclination: | 89.8828° |
| perigee height: | 1061 km |
| apogee height: | 1160 km |
| right ascension of ascending node: | 252.8198° |
| argument of perigee: | 12.3731° |
| revolutions per day: | 13.39625596 |
| mean anomaly at epoch: | 112.3857° |
| orbit number at epoch: | 77384 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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