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 66356U 26144.98155488 +.00000000 +00000-0 +84228-3 0 00001
2 66356 53.1585 238.2741 0001199 86.0625 274.0512 15.30205929 06
| Epoch (UTC): | 24 May 2026 23:33:26 |
| Eccentricity: | 0.0001199 |
| inclination: | 53.1585° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 238.2741° |
| argument of perigee: | 86.0625° |
| revolutions per day: | 15.30205929 |
| mean anomaly at epoch: | 274.0512° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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