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 66921U 26145.49684301 +.00000000 +00000-0 +57655-4 0 00002
2 66921 50.0117 227.2588 0001009 214.2712 145.8095 13.29325456 05
| Epoch (UTC): | 25 May 2026 11:55:27 |
| Eccentricity: | 0.0001009 |
| inclination: | 50.0117° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 227.2588° |
| argument of perigee: | 214.2712° |
| revolutions per day: | 13.29325456 |
| mean anomaly at epoch: | 145.8095° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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