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 64595U 26145.24837315 +.00000000 +00000-0 +41218-3 0 00002
2 64595 53.1603 339.8222 0001837 77.0287 283.0919 15.30206242 05
| Epoch (UTC): | 25 May 2026 05:57:39 |
| Eccentricity: | 0.0001837 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 339.8222° |
| argument of perigee: | 77.0287° |
| revolutions per day: | 15.30206242 |
| mean anomaly at epoch: | 283.0919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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