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 66713U 26145.63257756 +.00000000 +00000-0 +28085-3 0 00001
2 66713 97.4194 219.4998 0006150 86.9609 273.2330 15.19529479 03
| Epoch (UTC): | 25 May 2026 15:10:54 |
| Eccentricity: | 0.0006150 |
| inclination: | 97.4194° |
| perigee height: | 503 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 219.4998° |
| argument of perigee: | 86.9609° |
| revolutions per day: | 15.19529479 |
| mean anomaly at epoch: | 273.2330° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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