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 66037U 26145.48242214 +.00000000 +00000-0 +18619-3 0 00008
2 66037 89.0024 44.9532 0001980 69.3601 290.7762 13.51007402 03
| Epoch (UTC): | 25 May 2026 11:34:41 |
| Eccentricity: | 0.0001980 |
| inclination: | 89.0024° |
| perigee height: | 1067 km |
| apogee height: | 1070 km |
| right ascension of ascending node: | 44.9532° |
| argument of perigee: | 69.3601° |
| revolutions per day: | 13.51007402 |
| mean anomaly at epoch: | 290.7762° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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