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 66050U 26145.46592632 +.00000000 +00000-0 +18487-3 0 00006
2 66050 89.0020 45.4699 0001977 81.5751 278.5625 13.51007042 04
| Epoch (UTC): | 25 May 2026 11:10:56 |
| Eccentricity: | 0.0001977 |
| inclination: | 89.0020° |
| perigee height: | 1067 km |
| apogee height: | 1070 km |
| right ascension of ascending node: | 45.4699° |
| argument of perigee: | 81.5751° |
| revolutions per day: | 13.51007042 |
| mean anomaly at epoch: | 278.5625° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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