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 66936U 26145.30596125 +.00000000 +00000-0 +56898-3 0 00001
2 66936 53.1595 2.1118 0001411 98.2225 261.8937 15.34397708 01
| Epoch (UTC): | 25 May 2026 07:20:35 |
| Eccentricity: | 0.0001411 |
| inclination: | 53.1595° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 2.1118° |
| argument of perigee: | 98.2225° |
| revolutions per day: | 15.34397708 |
| mean anomaly at epoch: | 261.8937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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