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 55600U 26145.08033692 +.00000000 +00000-0 +72111-5 0 00005
2 55600 43.0020 282.6981 0000987 279.3430 80.7310 15.27577709 04
| Epoch (UTC): | 25 May 2026 01:55:41 |
| Eccentricity: | 0.0000987 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 282.6981° |
| argument of perigee: | 279.3430° |
| revolutions per day: | 15.27577709 |
| mean anomaly at epoch: | 80.7310° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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