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 66098U 26145.61981052 +.00000000 +00000-0 +70081-3 0 00001
2 66098 53.1594 106.4893 0002049 104.3418 255.7812 15.34400629 09
| Epoch (UTC): | 25 May 2026 14:52:31 |
| Eccentricity: | 0.0002049 |
| inclination: | 53.1594° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 106.4893° |
| argument of perigee: | 104.3418° |
| revolutions per day: | 15.34400629 |
| mean anomaly at epoch: | 255.7812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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