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 49055U 26144.43697291 +.00000000 +00000-0 +00000-0 0 00004
2 49055 0.0101 303.2052 0001490 138.4492 247.6149 1.00265819 02
| Epoch (UTC): | 24 May 2026 10:29:14 |
| Eccentricity: | 0.0001490 |
| inclination: | 0.0101° |
| perigee height: | 35782 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 303.2052° |
| argument of perigee: | 138.4492° |
| revolutions per day: | 1.00265819 |
| mean anomaly at epoch: | 247.6149° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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