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 23082.88576319 .00000405 00000-0 16940-3 0 9994
2 22827 98.8043 129.1399 0007947 254.8476 278.4485 14.31590158539240
| Epoch (UTC): | 23 March 2023 21:15:29 |
| Eccentricity: | 0.0007947 |
| inclination: | 98.8043° |
| perigee height: | 781 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 129.1399° |
| argument of perigee: | 254.8476° |
| revolutions per day: | 14.31590158 |
| mean anomaly at epoch: | 278.4485° |
| orbit number at epoch: | 53924 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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