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 49086U 26145.31702341 +.00000000 +00000-0 -38652-3 0 00007
2 49086 87.8948 355.2276 0001855 89.3015 270.8327 13.12443319 08
| Epoch (UTC): | 25 May 2026 07:36:30 |
| Eccentricity: | 0.0001855 |
| inclination: | 87.8948° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2276° |
| argument of perigee: | 89.3015° |
| revolutions per day: | 13.12443319 |
| mean anomaly at epoch: | 270.8327° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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