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 66549U 26145.39297729 +.00000000 +00000-0 +00000-0 0 00009
2 66549 4.5955 272.4958 0000849 28.2510 200.5604 1.00276032 04
| Epoch (UTC): | 25 May 2026 09:25:53 |
| Eccentricity: | 0.0000849 |
| inclination: | 4.5955° |
| perigee height: | 35782 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 272.4958° |
| argument of perigee: | 28.2510° |
| revolutions per day: | 1.00276032 |
| mean anomaly at epoch: | 200.5604° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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