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 64010U 26145.39792609 +.00000000 +00000-0 +60939-3 0 00007
2 64010 42.9970 285.0278 0000828 300.0723 60.0047 15.27591170 04
| Epoch (UTC): | 25 May 2026 09:33:00 |
| Eccentricity: | 0.0000828 |
| inclination: | 42.9970° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 285.0278° |
| argument of perigee: | 300.0723° |
| revolutions per day: | 15.27591170 |
| mean anomaly at epoch: | 60.0047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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