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 64068U 26145.62589022 +.00000000 +00000-0 +16316-2 0 00008
2 64068 43.0003 354.8894 0001950 274.7932 85.2713 15.70910153 04
| Epoch (UTC): | 25 May 2026 15:01:16 |
| Eccentricity: | 0.0001950 |
| inclination: | 43.0003° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 354.8894° |
| argument of perigee: | 274.7932° |
| revolutions per day: | 15.70910153 |
| mean anomaly at epoch: | 85.2713° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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