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 64422U 26145.53545454 +.00000000 +00000-0 +25011-3 0 00006
2 64422 70.0007 240.8758 0003905 268.4997 91.5715 14.98335542 02
| Epoch (UTC): | 25 May 2026 12:51:03 |
| Eccentricity: | 0.0003905 |
| inclination: | 70.0007° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 240.8758° |
| argument of perigee: | 268.4997° |
| revolutions per day: | 14.98335542 |
| mean anomaly at epoch: | 91.5715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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