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 56784U 26145.34849913 +.00000000 +00000-0 -62251-5 0 00004
2 56784 69.9986 131.2781 0003672 266.3808 93.6931 14.98330628 08
| Epoch (UTC): | 25 May 2026 08:21:50 |
| Eccentricity: | 0.0003672 |
| inclination: | 69.9986° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 131.2781° |
| argument of perigee: | 266.3808° |
| revolutions per day: | 14.98330628 |
| mean anomaly at epoch: | 93.6931° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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