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 66573U 26144.77875600 +.00000000 +00000-0 +60894-3 0 00007
2 66573 42.9994 277.6135 0001832 283.7401 76.3247 15.27595050 04
| Epoch (UTC): | 24 May 2026 18:41:24 |
| Eccentricity: | 0.0001832 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.6135° |
| argument of perigee: | 283.7401° |
| revolutions per day: | 15.27595050 |
| mean anomaly at epoch: | 76.3247° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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