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 64234U 26145.33685275 +.00000000 +00000-0 +15465-2 0 00002
2 64234 43.0005 107.6187 0000931 259.3058 100.7705 15.70894793 01
| Epoch (UTC): | 25 May 2026 08:05:04 |
| Eccentricity: | 0.0000931 |
| inclination: | 43.0005° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 107.6187° |
| argument of perigee: | 259.3058° |
| revolutions per day: | 15.70894793 |
| mean anomaly at epoch: | 100.7705° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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