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 64293U 26145.34489390 +.00000000 +00000-0 +28530-3 0 00006
2 64293 70.0021 1.0683 0002320 268.9289 91.1605 14.98339538 00
| Epoch (UTC): | 25 May 2026 08:16:38 |
| Eccentricity: | 0.0002320 |
| inclination: | 70.0021° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 1.0683° |
| argument of perigee: | 268.9289° |
| revolutions per day: | 14.98339538 |
| mean anomaly at epoch: | 91.1605° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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