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 66703U 26145.62998985 +.00000000 +00000-0 +32786-3 0 00008
2 66703 97.4123 220.8567 0000645 29.0749 331.0527 15.29189406 02
| Epoch (UTC): | 25 May 2026 15:07:11 |
| Eccentricity: | 0.0000645 |
| inclination: | 97.4123° |
| perigee height: | 478 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 220.8567° |
| argument of perigee: | 29.0749° |
| revolutions per day: | 15.29189406 |
| mean anomaly at epoch: | 331.0527° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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