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 64135U 26144.66494983 +.00000000 +00000-0 +13559-2 0 00003
2 64135 43.0044 236.2852 0002873 267.8754 92.1785 15.70897480 04
| Epoch (UTC): | 24 May 2026 15:57:31 |
| Eccentricity: | 0.0002873 |
| inclination: | 43.0044° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 236.2852° |
| argument of perigee: | 267.8754° |
| revolutions per day: | 15.70897480 |
| mean anomaly at epoch: | 92.1785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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