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 10962U 26088.21655954 +.00000000 +00000-0 +93326-4 0 00009
2 10962 74.0782 53.9255 0025592 212.6950 147.2624 14.42855726 05
| Epoch (UTC): | 29 March 2026 05:11:50 |
| Eccentricity: | 0.0025592 |
| inclination: | 74.0782° |
| perigee height: | 731 km |
| apogee height: | 767 km |
| right ascension of ascending node: | 53.9255° |
| argument of perigee: | 212.6950° |
| revolutions per day: | 14.42855726 |
| mean anomaly at epoch: | 147.2624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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