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 64122U 26145.39279674 +.00000000 +00000-0 +40795-3 0 00001
2 64122 53.1603 29.9423 0001505 90.6165 269.5009 15.31717785 08
| Epoch (UTC): | 25 May 2026 09:25:37 |
| Eccentricity: | 0.0001505 |
| inclination: | 53.1603° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 29.9423° |
| argument of perigee: | 90.6165° |
| revolutions per day: | 15.31717785 |
| mean anomaly at epoch: | 269.5009° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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