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 64830U 26145.53609551 +.00000000 +00000-0 +19514-3 0 00009
2 64830 51.9030 325.7669 0000739 101.5081 258.5964 14.79918042 08
| Epoch (UTC): | 25 May 2026 12:51:58 |
| Eccentricity: | 0.0000739 |
| inclination: | 51.9030° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 325.7669° |
| argument of perigee: | 101.5081° |
| revolutions per day: | 14.79918042 |
| mean anomaly at epoch: | 258.5964° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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