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 66198U 26145.27078742 +.00000000 +00000-0 +57137-3 0 00004
2 66198 53.1599 249.8976 0001389 84.6787 275.4372 15.30200484 07
| Epoch (UTC): | 25 May 2026 06:29:56 |
| Eccentricity: | 0.0001389 |
| inclination: | 53.1599° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 249.8976° |
| argument of perigee: | 84.6787° |
| revolutions per day: | 15.30200484 |
| mean anomaly at epoch: | 275.4372° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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