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 66204U 26145.57097622 +.00000000 +00000-0 +36262-3 0 00009
2 66204 53.1588 248.2170 0000815 61.3757 298.7326 15.30189240 07
| Epoch (UTC): | 25 May 2026 13:42:12 |
| Eccentricity: | 0.0000815 |
| inclination: | 53.1588° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.2170° |
| argument of perigee: | 61.3757° |
| revolutions per day: | 15.30189240 |
| mean anomaly at epoch: | 298.7326° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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