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 11751U 26088.23481602 +.00000000 +00000-0 +84274-4 0 00007
2 11751 65.8386 110.6368 0014095 320.7597 110.3412 13.77344914 05
| Epoch (UTC): | 29 March 2026 05:38:08 |
| Eccentricity: | 0.0014095 |
| inclination: | 65.8386° |
| perigee height: | 963 km |
| apogee height: | 984 km |
| right ascension of ascending node: | 110.6368° |
| argument of perigee: | 320.7597° |
| revolutions per day: | 13.77344914 |
| mean anomaly at epoch: | 110.3412° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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