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 64071U 26145.62497588 +.00000000 +00000-0 +21432-2 0 00002
2 64071 43.0009 354.8791 0001752 256.4915 103.5758 15.70931340 02
| Epoch (UTC): | 25 May 2026 14:59:57 |
| Eccentricity: | 0.0001752 |
| inclination: | 43.0009° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 354.8791° |
| argument of perigee: | 256.4915° |
| revolutions per day: | 15.70931340 |
| mean anomaly at epoch: | 103.5758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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