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 66771U 26145.11356455 +.00000000 +00000-0 +23465-3 0 00001
2 66771 97.4238 219.3792 0001135 33.9141 326.2167 15.20439303 03
| Epoch (UTC): | 25 May 2026 02:43:31 |
| Eccentricity: | 0.0001135 |
| inclination: | 97.4238° |
| perigee height: | 504 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 219.3792° |
| argument of perigee: | 33.9141° |
| revolutions per day: | 15.20439303 |
| mean anomaly at epoch: | 326.2167° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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