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 66524U 26145.22200668 +.00000000 +00000-0 +47048-3 0 00006
2 66524 42.9996 206.1070 0001497 263.6774 96.3907 15.27589300 00
| Epoch (UTC): | 25 May 2026 05:19:41 |
| Eccentricity: | 0.0001497 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 206.1070° |
| argument of perigee: | 263.6774° |
| revolutions per day: | 15.27589300 |
| mean anomaly at epoch: | 96.3907° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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