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 64870U 26145.46098799 +.00000000 +00000-0 +15674-3 0 00004
2 64870 97.6701 209.6594 0004838 349.3443 10.7674 14.93395778 06
| Epoch (UTC): | 25 May 2026 11:03:49 |
| Eccentricity: | 0.0004838 |
| inclination: | 97.6701° |
| perigee height: | 584 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 209.6594° |
| argument of perigee: | 349.3443° |
| revolutions per day: | 14.93395778 |
| mean anomaly at epoch: | 10.7674° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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