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 20578U 26159.54326096 +.00000000 +00000-0 +78410-4 0 00007
2 20578 82.9435 85.7545 0013063 163.2110 15.7718 13.76652464 09
| Epoch (UTC): | 08 June 2026 13:02:17 |
| Eccentricity: | 0.0013063 |
| inclination: | 82.9435° |
| perigee height: | 966 km |
| apogee height: | 985 km |
| right ascension of ascending node: | 85.7545° |
| argument of perigee: | 163.2110° |
| revolutions per day: | 13.76652464 |
| mean anomaly at epoch: | 15.7718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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