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 27609U 02058E 22272.25201209 .00000280 00000-0 56753-4 0 9995
2 27609 64.5564 194.5861 0053255 253.9373 105.5862 14.78793270 66863
| Epoch (UTC): | 29 September 2022 06:02:53 |
| Eccentricity: | 0.0053255 |
| inclination: | 64.5564° |
| perigee height: | 596 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 194.5861° |
| argument of perigee: | 253.9373° |
| revolutions per day: | 14.78793270 |
| mean anomaly at epoch: | 105.5862° |
| orbit number at epoch: | 6686 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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