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 47266U 26145.12911992 +.00000000 +00000-0 -32336-5 0 00003
2 47266 87.8950 355.2580 0001626 89.8721 270.2594 13.12441352 07
| Epoch (UTC): | 25 May 2026 03:05:55 |
| Eccentricity: | 0.0001626 |
| inclination: | 87.8950° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2580° |
| argument of perigee: | 89.8721° |
| revolutions per day: | 13.12441352 |
| mean anomaly at epoch: | 270.2594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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