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 22022.44647071 .00000410 00000-0 78086-4 0 9996
2 27607 64.5554 28.6017 0067180 323.9016 35.7559 14.75881556 26825
| Epoch (UTC): | 22 January 2022 10:42:55 |
| Eccentricity: | 0.0067180 |
| inclination: | 64.5554° |
| perigee height: | 595 km |
| apogee height: | 689 km |
| right ascension of ascending node: | 28.6017° |
| argument of perigee: | 323.9016° |
| revolutions per day: | 14.75881556 |
| mean anomaly at epoch: | 35.7559° |
| orbit number at epoch: | 2682 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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