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 64368U 26145.56002235 +.00000000 +00000-0 +31660-3 0 00000
2 64368 70.0005 200.7405 0003924 267.2534 92.8176 14.98338087 00
| Epoch (UTC): | 25 May 2026 13:26:25 |
| Eccentricity: | 0.0003924 |
| inclination: | 70.0005° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 200.7405° |
| argument of perigee: | 267.2534° |
| revolutions per day: | 14.98338087 |
| mean anomaly at epoch: | 92.8176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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