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 26087.87806223 +.00000000 +00000-0 +47946-5 0 00009
2 20578 82.9433 138.9922 0013102 16.7180 155.6291 13.76637529 05
| Epoch (UTC): | 28 March 2026 21:04:24 |
| Eccentricity: | 0.0013102 |
| inclination: | 82.9433° |
| perigee height: | 966 km |
| apogee height: | 985 km |
| right ascension of ascending node: | 138.9922° |
| argument of perigee: | 16.7180° |
| revolutions per day: | 13.76637529 |
| mean anomaly at epoch: | 155.6291° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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