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 64035U 26145.36918043 +.00000000 +00000-0 +39252-3 0 00007
2 64035 70.0006 281.1721 0003062 266.6888 93.3921 14.98341416 08
| Epoch (UTC): | 25 May 2026 08:51:37 |
| Eccentricity: | 0.0003062 |
| inclination: | 70.0006° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 281.1721° |
| argument of perigee: | 266.6888° |
| revolutions per day: | 14.98341416 |
| mean anomaly at epoch: | 93.3921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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