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 55377U 26145.54011463 +.00000000 +00000-0 +39235-4 0 00008
2 55377 43.0035 244.3370 0001817 277.9513 82.1133 15.27575791 05
| Epoch (UTC): | 25 May 2026 12:57:45 |
| Eccentricity: | 0.0001817 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 244.3370° |
| argument of perigee: | 277.9513° |
| revolutions per day: | 15.27575791 |
| mean anomaly at epoch: | 82.1133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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