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 55616U 26144.87904573 +.00000000 +00000-0 +50633-4 0 00007
2 55616 43.0002 283.7665 0001483 251.9818 108.0872 15.27594032 05
| Epoch (UTC): | 24 May 2026 21:05:49 |
| Eccentricity: | 0.0001483 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 283.7665° |
| argument of perigee: | 251.9818° |
| revolutions per day: | 15.27594032 |
| mean anomaly at epoch: | 108.0872° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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