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 66049U 26145.46178598 +.00000000 +00000-0 +18738-3 0 00004
2 66049 89.0029 45.4810 0002140 70.1072 290.0310 13.51005876 02
| Epoch (UTC): | 25 May 2026 11:04:58 |
| Eccentricity: | 0.0002140 |
| inclination: | 89.0029° |
| perigee height: | 1067 km |
| apogee height: | 1070 km |
| right ascension of ascending node: | 45.4810° |
| argument of perigee: | 70.1072° |
| revolutions per day: | 13.51005876 |
| mean anomaly at epoch: | 290.0310° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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