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 64811U 26145.41929626 +.00000000 +00000-0 -12279-3 0 00005
2 64811 70.0004 300.8481 0002781 268.6113 91.4728 14.98326601 03
| Epoch (UTC): | 25 May 2026 10:03:47 |
| Eccentricity: | 0.0002781 |
| inclination: | 70.0004° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 300.8481° |
| argument of perigee: | 268.6113° |
| revolutions per day: | 14.98326601 |
| mean anomaly at epoch: | 91.4728° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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