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 66200U 26145.55514610 +.00000000 +00000-0 +89457-3 0 00008
2 66200 53.1588 248.1160 0000790 84.5334 275.5757 15.30202767 02
| Epoch (UTC): | 25 May 2026 13:19:24 |
| Eccentricity: | 0.0000790 |
| inclination: | 53.1588° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.1160° |
| argument of perigee: | 84.5334° |
| revolutions per day: | 15.30202767 |
| mean anomaly at epoch: | 275.5757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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