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 66695U 26145.44357992 +.00000000 +00000-0 +23945-3 0 00002
2 66695 97.4202 219.6100 0002174 77.8991 282.2488 15.20574033 06
| Epoch (UTC): | 25 May 2026 10:38:45 |
| Eccentricity: | 0.0002174 |
| inclination: | 97.4202° |
| perigee height: | 503 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 219.6100° |
| argument of perigee: | 77.8991° |
| revolutions per day: | 15.20574033 |
| mean anomaly at epoch: | 282.2488° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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