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 66689U 26145.44863699 +.00000000 +00000-0 +10338-3 0 00003
2 66689 97.4211 219.1774 0004474 92.7142 267.4604 15.18110827 09
| Epoch (UTC): | 25 May 2026 10:46:02 |
| Eccentricity: | 0.0004474 |
| inclination: | 97.4211° |
| perigee height: | 508 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 219.1774° |
| argument of perigee: | 92.7142° |
| revolutions per day: | 15.18110827 |
| mean anomaly at epoch: | 267.4604° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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