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 66775U 26145.46823671 +.00000000 +00000-0 +28331-3 0 00009
2 66775 97.4136 219.5841 0001298 162.5236 197.6045 15.20982867 08
| Epoch (UTC): | 25 May 2026 11:14:15 |
| Eccentricity: | 0.0001298 |
| inclination: | 97.4136° |
| perigee height: | 502 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 219.5841° |
| argument of perigee: | 162.5236° |
| revolutions per day: | 15.20982867 |
| mean anomaly at epoch: | 197.6045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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