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 64042U 26145.36902435 +.00000000 +00000-0 +50414-3 0 00006
2 64042 70.0003 281.2913 0003228 268.4995 91.5794 14.98343530 07
| Epoch (UTC): | 25 May 2026 08:51:23 |
| Eccentricity: | 0.0003228 |
| inclination: | 70.0003° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 281.2913° |
| argument of perigee: | 268.4995° |
| revolutions per day: | 14.98343530 |
| mean anomaly at epoch: | 91.5794° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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