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 36585U 26143.78349725 +.00000000 +00000-0 +00000-0 0 00001
2 36585 54.2724 209.5453 0126358 66.1078 118.5533 2.00561193 07
| Epoch (UTC): | 23 May 2026 18:48:14 |
| Eccentricity: | 0.0126358 |
| inclination: | 54.2724° |
| perigee height: | 19847 km |
| apogee height: | 20518 km |
| right ascension of ascending node: | 209.5453° |
| argument of perigee: | 66.1078° |
| revolutions per day: | 2.00561193 |
| mean anomaly at epoch: | 118.5533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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