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 10514U 26088.15699264 +.00000000 +00000-0 +64425-4 0 00005
2 10514 81.2071 324.6117 0023028 199.0661 160.9651 14.11222504 03
| Epoch (UTC): | 29 March 2026 03:46:04 |
| Eccentricity: | 0.0023028 |
| inclination: | 81.2071° |
| perigee height: | 839 km |
| apogee height: | 872 km |
| right ascension of ascending node: | 324.6117° |
| argument of perigee: | 199.0661° |
| revolutions per day: | 14.11222504 |
| mean anomaly at epoch: | 160.9651° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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