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 65574U 26145.41723484 +.00000000 +00000-0 +11350-3 0 00004
2 65574 81.3029 31.9926 0004651 267.4593 92.6031 13.83305996 02
| Epoch (UTC): | 25 May 2026 10:00:49 |
| Eccentricity: | 0.0004651 |
| inclination: | 81.3029° |
| perigee height: | 949 km |
| apogee height: | 956 km |
| right ascension of ascending node: | 31.9926° |
| argument of perigee: | 267.4593° |
| revolutions per day: | 13.83305996 |
| mean anomaly at epoch: | 92.6031° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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