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 22220U 92076B 24357.59642510 .00000127 00000-0 87305-4 0 9992
2 22220 71.0010 39.5682 0011179 40.3286 72.6724 14.16752262659211
| Epoch (UTC): | 22 December 2024 14:18:51 |
| Eccentricity: | 0.0011179 |
| inclination: | 71.0010° |
| perigee height: | 828 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 39.5682° |
| argument of perigee: | 40.3286° |
| revolutions per day: | 14.16752262 |
| mean anomaly at epoch: | 72.6724° |
| orbit number at epoch: | 65921 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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