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 64684U 26145.23549794 +.00000000 +00000-0 +11629-2 0 00003
2 64684 53.1584 130.7777 0001181 96.3214 263.7923 15.34423293 02
| Epoch (UTC): | 25 May 2026 05:39:07 |
| Eccentricity: | 0.0001181 |
| inclination: | 53.1584° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 130.7777° |
| argument of perigee: | 96.3214° |
| revolutions per day: | 15.34423293 |
| mean anomaly at epoch: | 263.7923° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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