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 66913U 26145.41180471 +.00000000 +00000-0 +89474-4 0 00008
2 66913 80.4047 313.1124 0010557 301.5088 58.5041 13.97336311 08
| Epoch (UTC): | 25 May 2026 09:52:59 |
| Eccentricity: | 0.0010557 |
| inclination: | 80.4047° |
| perigee height: | 895 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 313.1124° |
| argument of perigee: | 301.5088° |
| revolutions per day: | 13.97336311 |
| mean anomaly at epoch: | 58.5041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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