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 64793U 26145.40696775 +.00000000 +00000-0 +15336-3 0 00005
2 64793 70.0007 301.2074 0003058 264.3806 95.7004 14.98336916 02
| Epoch (UTC): | 25 May 2026 09:46:02 |
| Eccentricity: | 0.0003058 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 301.2074° |
| argument of perigee: | 264.3806° |
| revolutions per day: | 14.98336916 |
| mean anomaly at epoch: | 95.7004° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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