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 64348U 26145.43902400 +.00000000 +00000-0 +23628-3 0 00002
2 64348 70.0005 201.1282 0003794 267.4198 92.6527 14.98336989 06
| Epoch (UTC): | 25 May 2026 10:32:11 |
| Eccentricity: | 0.0003794 |
| inclination: | 70.0005° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 201.1282° |
| argument of perigee: | 267.4198° |
| revolutions per day: | 14.98336989 |
| mean anomaly at epoch: | 92.6527° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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