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 24277U 96046A 22143.87675373 .00000194 00000-0 94280-4 0 9996
2 24277 98.9339 146.1168 0002218 104.3095 255.8332 14.29536435343399
| Epoch (UTC): | 23 May 2022 21:02:31 |
| Eccentricity: | 0.0002218 |
| inclination: | 98.9339° |
| perigee height: | 791 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 146.1168° |
| argument of perigee: | 104.3095° |
| revolutions per day: | 14.29536435 |
| mean anomaly at epoch: | 255.8332° |
| orbit number at epoch: | 34339 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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