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 66751U 26145.44261927 +.00000000 +00000-0 +56645-4 0 00001
2 66751 97.4213 219.3357 0004687 69.8156 290.3581 15.17725271 09
| Epoch (UTC): | 25 May 2026 10:37:22 |
| Eccentricity: | 0.0004687 |
| inclination: | 97.4213° |
| perigee height: | 509 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 219.3357° |
| argument of perigee: | 69.8156° |
| revolutions per day: | 15.17725271 |
| mean anomaly at epoch: | 290.3581° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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