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 66661U 26145.54190970 +.00000000 +00000-0 +17216-3 0 00001
2 66661 97.7486 75.3230 0016228 94.5517 265.7557 14.93908793 08
| Epoch (UTC): | 25 May 2026 13:00:20 |
| Eccentricity: | 0.0016228 |
| inclination: | 97.7486° |
| perigee height: | 574 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 75.3230° |
| argument of perigee: | 94.5517° |
| revolutions per day: | 14.93908793 |
| mean anomaly at epoch: | 265.7557° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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