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 66035U 26145.48650681 +.00000000 +00000-0 +19209-3 0 00003
2 66035 89.0030 45.5043 0002164 68.9102 291.2280 13.51007732 05
| Epoch (UTC): | 25 May 2026 11:40:34 |
| Eccentricity: | 0.0002164 |
| inclination: | 89.0030° |
| perigee height: | 1067 km |
| apogee height: | 1070 km |
| right ascension of ascending node: | 45.5043° |
| argument of perigee: | 68.9102° |
| revolutions per day: | 13.51007732 |
| mean anomaly at epoch: | 291.2280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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