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 66649U 26145.40620186 +.00000000 +00000-0 +85575-4 0 00003
2 66649 82.5034 184.7908 0014626 251.2708 108.6785 12.42896702 02
| Epoch (UTC): | 25 May 2026 09:44:55 |
| Eccentricity: | 0.0014626 |
| inclination: | 82.5034° |
| perigee height: | 1483 km |
| apogee height: | 1506 km |
| right ascension of ascending node: | 184.7908° |
| argument of perigee: | 251.2708° |
| revolutions per day: | 12.42896702 |
| mean anomaly at epoch: | 108.6785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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