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 25198.75565110 .00000068 00000-0 57659-4 0 9997
2 22220 71.0018 323.2396 0010626 93.6739 65.3053 14.16811878688556
| Epoch (UTC): | 17 July 2025 18:08:08 |
| Eccentricity: | 0.0010626 |
| inclination: | 71.0018° |
| perigee height: | 828 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 323.2396° |
| argument of perigee: | 93.6739° |
| revolutions per day: | 14.16811878 |
| mean anomaly at epoch: | 65.3053° |
| orbit number at epoch: | 68855 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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