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 66044U 26145.21902479 +.00000000 +00000-0 +17746-3 0 00003
2 66044 89.0024 45.4209 0002053 73.4191 286.7185 13.51006315 06
| Epoch (UTC): | 25 May 2026 05:15:23 |
| Eccentricity: | 0.0002053 |
| inclination: | 89.0024° |
| perigee height: | 1067 km |
| apogee height: | 1070 km |
| right ascension of ascending node: | 45.4209° |
| argument of perigee: | 73.4191° |
| revolutions per day: | 13.51006315 |
| mean anomaly at epoch: | 286.7185° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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