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 66726U 26145.44435417 +.00000000 +00000-0 +29004-3 0 00008
2 66726 97.4244 219.4052 0006080 82.6884 277.5042 15.19439989 07
| Epoch (UTC): | 25 May 2026 10:39:52 |
| Eccentricity: | 0.0006080 |
| inclination: | 97.4244° |
| perigee height: | 503 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 219.4052° |
| argument of perigee: | 82.6884° |
| revolutions per day: | 15.19439989 |
| mean anomaly at epoch: | 277.5042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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