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 65420U 26145.53211084 +.00000000 +00000-0 +39423-3 0 00006
2 65420 53.1571 235.1134 0001105 87.4680 272.6448 15.31700631 00
| Epoch (UTC): | 25 May 2026 12:46:14 |
| Eccentricity: | 0.0001105 |
| inclination: | 53.1571° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 235.1134° |
| argument of perigee: | 87.4680° |
| revolutions per day: | 15.31700631 |
| mean anomaly at epoch: | 272.6448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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