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 66672U 26145.43937551 +.00000000 +00000-0 +13906-3 0 00007
2 66672 97.4198 218.9981 0008456 83.9313 276.2884 15.17816080 09
| Epoch (UTC): | 25 May 2026 10:32:42 |
| Eccentricity: | 0.0008456 |
| inclination: | 97.4198° |
| perigee height: | 507 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 218.9981° |
| argument of perigee: | 83.9313° |
| revolutions per day: | 15.17816080 |
| mean anomaly at epoch: | 276.2884° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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