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 66030U 26145.33335647 +.00000000 +00000-0 +20056-2 0 00005
2 66030 53.1580 108.0741 0001281 87.7693 53.4649 15.30170404 08
| Epoch (UTC): | 25 May 2026 08:00:01 |
| Eccentricity: | 0.0001281 |
| inclination: | 53.1580° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 108.0741° |
| argument of perigee: | 87.7693° |
| revolutions per day: | 15.30170404 |
| mean anomaly at epoch: | 53.4649° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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