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 10521U 26088.15104779 +.00000000 +00000-0 +72843-4 0 00008
2 10521 74.0242 87.3804 0019448 35.2858 324.9581 14.42403972 05
| Epoch (UTC): | 29 March 2026 03:37:30 |
| Eccentricity: | 0.0019448 |
| inclination: | 74.0242° |
| perigee height: | 737 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 87.3804° |
| argument of perigee: | 35.2858° |
| revolutions per day: | 14.42403972 |
| mean anomaly at epoch: | 324.9581° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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