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 66536U 26145.46427019 +.00000000 +00000-0 +12021-4 0 00000
2 66536 42.9992 204.4768 0001523 275.3696 84.6982 15.27567470 04
| Epoch (UTC): | 25 May 2026 11:08:32 |
| Eccentricity: | 0.0001523 |
| inclination: | 42.9992° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.4768° |
| argument of perigee: | 275.3696° |
| revolutions per day: | 15.27567470 |
| mean anomaly at epoch: | 84.6982° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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