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 66038U 26145.43301657 +.00000000 +00000-0 +18188-3 0 00002
2 66038 89.0022 45.5020 0002062 66.9606 293.1763 13.51006546 07
| Epoch (UTC): | 25 May 2026 10:23:32 |
| Eccentricity: | 0.0002062 |
| inclination: | 89.0022° |
| perigee height: | 1067 km |
| apogee height: | 1070 km |
| right ascension of ascending node: | 45.5020° |
| argument of perigee: | 66.9606° |
| revolutions per day: | 13.51006546 |
| mean anomaly at epoch: | 293.1763° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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