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 64502U 26145.33070301 +.00000000 +00000-0 +58100-3 0 00002
2 64502 51.8997 266.6712 0000330 141.3893 218.7093 14.79932350 06
| Epoch (UTC): | 25 May 2026 07:56:12 |
| Eccentricity: | 0.0000330 |
| inclination: | 51.8997° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 266.6712° |
| argument of perigee: | 141.3893° |
| revolutions per day: | 14.79932350 |
| mean anomaly at epoch: | 218.7093° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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