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 64318U 26145.42951417 +.00000000 +00000-0 +23046-2 0 00003
2 64318 42.9995 286.6466 0001826 265.6952 94.3707 15.70939370 06
| Epoch (UTC): | 25 May 2026 10:18:30 |
| Eccentricity: | 0.0001826 |
| inclination: | 42.9995° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 286.6466° |
| argument of perigee: | 265.6952° |
| revolutions per day: | 15.70939370 |
| mean anomaly at epoch: | 94.3707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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