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 66841U 26145.33835160 +.00000000 +00000-0 -12732-5 0 00006
2 66841 70.0010 141.3378 0003729 266.2272 93.8460 14.98325541 02
| Epoch (UTC): | 25 May 2026 08:07:13 |
| Eccentricity: | 0.0003729 |
| inclination: | 70.0010° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 141.3378° |
| argument of perigee: | 266.2272° |
| revolutions per day: | 14.98325541 |
| mean anomaly at epoch: | 93.8460° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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