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 55455U 26145.29898072 +.00000000 +00000-0 +18607-4 0 00006
2 55455 43.0052 256.4848 0002522 280.5294 79.5274 15.27576606 07
| Epoch (UTC): | 25 May 2026 07:10:31 |
| Eccentricity: | 0.0002522 |
| inclination: | 43.0052° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 256.4848° |
| argument of perigee: | 280.5294° |
| revolutions per day: | 15.27576606 |
| mean anomaly at epoch: | 79.5274° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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