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 64070U 26145.60904962 +.00000000 +00000-0 +12494-2 0 00006
2 64070 42.9996 354.7520 0001426 270.5304 89.5401 15.70894871 05
| Epoch (UTC): | 25 May 2026 14:37:01 |
| Eccentricity: | 0.0001426 |
| inclination: | 42.9996° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 354.7520° |
| argument of perigee: | 270.5304° |
| revolutions per day: | 15.70894871 |
| mean anomaly at epoch: | 89.5401° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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