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 66960U 26145.49985654 +.00000000 +00000-0 +52022-3 0 00002
2 66960 43.0003 309.7500 0000835 282.7788 77.2970 15.27596832 01
| Epoch (UTC): | 25 May 2026 11:59:47 |
| Eccentricity: | 0.0000835 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.7500° |
| argument of perigee: | 282.7788° |
| revolutions per day: | 15.27596832 |
| mean anomaly at epoch: | 77.2970° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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