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 is defined by the following mean orbital elements,
1 10520U 26100.16249007 +.00000000 +00000-0 +63358-4 0 00008
2 10520 74.0279 263.5064 0017136 157.4727 202.7183 14.37073596 04
| Epoch (UTC): | 10 April 2026 03:53:59 |
| Eccentricity: | 0.0017136 |
| inclination: | 74.0279° |
| perigee height: | 756 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 263.5064° |
| argument of perigee: | 157.4727° |
| revolutions per day: | 14.37073596 |
| mean anomaly at epoch: | 202.7183° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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