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 51649U 26145.60010969 +.00000000 +00000-0 -15050-3 0 00002
2 51649 87.9162 10.3471 0001786 88.2962 271.8374 13.17650302 03
| Epoch (UTC): | 25 May 2026 14:24:09 |
| Eccentricity: | 0.0001786 |
| inclination: | 87.9162° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.3471° |
| argument of perigee: | 88.2962° |
| revolutions per day: | 13.17650302 |
| mean anomaly at epoch: | 271.8374° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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