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 64594U 26144.77217333 +.00000000 +00000-0 +73077-3 0 00008
2 64594 53.1590 341.8322 0000973 96.1188 263.9923 15.30196611 05
| Epoch (UTC): | 24 May 2026 18:31:55 |
| Eccentricity: | 0.0000973 |
| inclination: | 53.1590° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 341.8322° |
| argument of perigee: | 96.1188° |
| revolutions per day: | 15.30196611 |
| mean anomaly at epoch: | 263.9923° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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