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 55365U 26145.63570936 +.00000000 +00000-0 -32055-4 0 00004
2 55365 43.0010 246.7610 0001378 276.4208 83.6487 15.27567129 09
| Epoch (UTC): | 25 May 2026 15:15:25 |
| Eccentricity: | 0.0001378 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 246.7610° |
| argument of perigee: | 276.4208° |
| revolutions per day: | 15.27567129 |
| mean anomaly at epoch: | 83.6487° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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