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 64601U 26145.54645260 +.00000000 +00000-0 +67931-3 0 00009
2 64601 53.1590 338.1249 0001111 82.9816 277.1311 15.30205819 06
| Epoch (UTC): | 25 May 2026 13:06:53 |
| Eccentricity: | 0.0001111 |
| inclination: | 53.1590° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.1249° |
| argument of perigee: | 82.9816° |
| revolutions per day: | 15.30205819 |
| mean anomaly at epoch: | 277.1311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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