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 66413U 26145.38430381 +.00000000 +00000-0 +91540-4 0 00004
2 66413 50.0029 17.6568 0001060 57.8862 302.2113 13.29323167 03
| Epoch (UTC): | 25 May 2026 09:13:23 |
| Eccentricity: | 0.0001060 |
| inclination: | 50.0029° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 17.6568° |
| argument of perigee: | 57.8862° |
| revolutions per day: | 13.29323167 |
| mean anomaly at epoch: | 302.2113° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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