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 66785U 26145.48469551 +.00000000 +00000-0 +54437-3 0 00001
2 66785 97.5283 217.1478 0005708 183.1394 176.9795 15.00045251 04
| Epoch (UTC): | 25 May 2026 11:37:57 |
| Eccentricity: | 0.0005708 |
| inclination: | 97.5283° |
| perigee height: | 563 km |
| apogee height: | 571 km |
| right ascension of ascending node: | 217.1478° |
| argument of perigee: | 183.1394° |
| revolutions per day: | 15.00045251 |
| mean anomaly at epoch: | 176.9795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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