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 66436U 26145.51081323 +.00000000 +00000-0 +58044-3 0 00003
2 66436 42.9970 200.1926 0001868 272.9610 87.1027 15.27565518 08
| Epoch (UTC): | 25 May 2026 12:15:34 |
| Eccentricity: | 0.0001868 |
| inclination: | 42.9970° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.1926° |
| argument of perigee: | 272.9610° |
| revolutions per day: | 15.27565518 |
| mean anomaly at epoch: | 87.1027° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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