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 66694U 26145.14063074 +.00000000 +00000-0 +28044-3 0 00008
2 66694 97.4219 218.2383 0009648 41.6926 318.5040 15.14689931 05
| Epoch (UTC): | 25 May 2026 03:22:30 |
| Eccentricity: | 0.0009648 |
| inclination: | 97.4219° |
| perigee height: | 515 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 218.2383° |
| argument of perigee: | 41.6926° |
| revolutions per day: | 15.14689931 |
| mean anomaly at epoch: | 318.5040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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