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 64516U 26145.52380061 +.00000000 +00000-0 +10384-3 0 00007
2 64516 51.9003 243.3706 0000324 103.0798 257.0201 14.79935221 04
| Epoch (UTC): | 25 May 2026 12:34:16 |
| Eccentricity: | 0.0000324 |
| inclination: | 51.9003° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 243.3706° |
| argument of perigee: | 103.0798° |
| revolutions per day: | 14.79935221 |
| mean anomaly at epoch: | 257.0201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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