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 64060U 26145.40211207 +.00000000 +00000-0 +56019-4 0 00009
2 64060 44.9831 123.5865 0012148 283.8982 76.0499 13.99127253 00
| Epoch (UTC): | 25 May 2026 09:39:02 |
| Eccentricity: | 0.0012148 |
| inclination: | 44.9831° |
| perigee height: | 888 km |
| apogee height: | 906 km |
| right ascension of ascending node: | 123.5865° |
| argument of perigee: | 283.8982° |
| revolutions per day: | 13.99127253 |
| mean anomaly at epoch: | 76.0499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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