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 64609U 26145.54963170 +.00000000 +00000-0 +27772-3 0 00009
2 64609 53.1587 338.1467 0001107 120.3231 239.7879 15.30178672 04
| Epoch (UTC): | 25 May 2026 13:11:28 |
| Eccentricity: | 0.0001107 |
| inclination: | 53.1587° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.1467° |
| argument of perigee: | 120.3231° |
| revolutions per day: | 15.30178672 |
| mean anomaly at epoch: | 239.7879° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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