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 64236U 26145.28906765 +.00000000 +00000-0 +17441-2 0 00004
2 64236 43.0018 107.2345 0001780 268.5936 91.4727 15.70909609 02
| Epoch (UTC): | 25 May 2026 06:56:15 |
| Eccentricity: | 0.0001780 |
| inclination: | 43.0018° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 107.2345° |
| argument of perigee: | 268.5936° |
| revolutions per day: | 15.70909609 |
| mean anomaly at epoch: | 91.4727° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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