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 27665U 03005C 22140.52825576 .00000208 00000-0 11566-3 0 9995
2 27665 39.5764 312.4364 0007101 75.6968 308.7070 14.28609965 8020
| Epoch (UTC): | 20 May 2022 12:40:41 |
| Eccentricity: | 0.0007101 |
| inclination: | 39.5764° |
| perigee height: | 791 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 312.4364° |
| argument of perigee: | 75.6968° |
| revolutions per day: | 14.28609965 |
| mean anomaly at epoch: | 308.7070° |
| orbit number at epoch: | 802 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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