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 64837U 26145.18087278 +.00000000 +00000-0 +48609-3 0 00000
2 64837 51.9014 312.3564 0000599 109.5988 250.5040 14.79941617 02
| Epoch (UTC): | 25 May 2026 04:20:27 |
| Eccentricity: | 0.0000599 |
| inclination: | 51.9014° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 312.3564° |
| argument of perigee: | 109.5988° |
| revolutions per day: | 14.79941617 |
| mean anomaly at epoch: | 250.5040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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