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 24284.53093532 .00000564 00000-0 30553-3 0 9996
2 22220 71.0008 193.4451 0012275 170.2749 2.2484 14.16715500648862
| Epoch (UTC): | 10 October 2024 12:44:32 |
| Eccentricity: | 0.0012275 |
| inclination: | 71.0008° |
| perigee height: | 827 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 193.4451° |
| argument of perigee: | 170.2749° |
| revolutions per day: | 14.16715500 |
| mean anomaly at epoch: | 2.2484° |
| orbit number at epoch: | 64886 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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