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 66652U 26145.53869969 +.00000000 +00000-0 +21072-3 0 00006
2 66652 97.7480 75.0149 0013360 75.5620 284.7081 14.92936418 03
| Epoch (UTC): | 25 May 2026 12:55:43 |
| Eccentricity: | 0.0013360 |
| inclination: | 97.7480° |
| perigee height: | 579 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 75.0149° |
| argument of perigee: | 75.5620° |
| revolutions per day: | 14.92936418 |
| mean anomaly at epoch: | 284.7081° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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