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 27607U 02058C 22178.55124407 .00000319 00000-0 64422-4 0 9990
2 27607 64.5549 271.0007 0078968 292.4854 66.7901 14.76144718 49865
| Epoch (UTC): | 27 June 2022 13:13:47 |
| Eccentricity: | 0.0078968 |
| inclination: | 64.5549° |
| perigee height: | 586 km |
| apogee height: | 697 km |
| right ascension of ascending node: | 271.0007° |
| argument of perigee: | 292.4854° |
| revolutions per day: | 14.76144718 |
| mean anomaly at epoch: | 66.7901° |
| orbit number at epoch: | 4986 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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