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 57386U 26087.02037537 +.00000000 +00000-0 +23802-4 0 00001
2 57386 99.5124 85.8423 0007026 22.1869 337.9654 15.06304834 05
| Epoch (UTC): | 28 March 2026 00:29:20 |
| Eccentricity: | 0.0007026 |
| inclination: | 99.5124° |
| perigee height: | 543 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 85.8423° |
| argument of perigee: | 22.1869° |
| revolutions per day: | 15.06304834 |
| mean anomaly at epoch: | 337.9654° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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