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 22827U 93061E 23273.89277914 .00000303 00000-0 13050-3 0 9992
2 22827 98.7808 322.5672 0009856 61.3756 112.0888 14.31706209566576
| Epoch (UTC): | 30 September 2023 21:25:36 |
| Eccentricity: | 0.0009856 |
| inclination: | 98.7808° |
| perigee height: | 779 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 322.5672° |
| argument of perigee: | 61.3756° |
| revolutions per day: | 14.31706209 |
| mean anomaly at epoch: | 112.0888° |
| orbit number at epoch: | 56657 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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