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 64036U 26145.35666170 +.00000000 +00000-0 +17488-3 0 00005
2 64036 70.0009 281.2430 0003049 268.9477 91.1333 14.98338062 00
| Epoch (UTC): | 25 May 2026 08:33:35 |
| Eccentricity: | 0.0003049 |
| inclination: | 70.0009° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 281.2430° |
| argument of perigee: | 268.9477° |
| revolutions per day: | 14.98338062 |
| mean anomaly at epoch: | 91.1333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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