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 27688U 99057MU 22333.56844103 .00000903 00000-0 25820-3 0 9997
2 27688 98.6521 356.0553 0090780 215.2417 299.9037 14.45296500539548
| Epoch (UTC): | 29 November 2022 13:38:33 |
| Eccentricity: | 0.0090780 |
| inclination: | 98.6521° |
| perigee height: | 676 km |
| apogee height: | 805 km |
| right ascension of ascending node: | 356.0553° |
| argument of perigee: | 215.2417° |
| revolutions per day: | 14.45296500 |
| mean anomaly at epoch: | 299.9037° |
| orbit number at epoch: | 53954 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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