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 65558U 26145.39549421 +.00000000 +00000-0 +18716-3 0 00003
2 65558 49.9795 144.6066 0008436 183.3104 176.7780 14.84073834 00
| Epoch (UTC): | 25 May 2026 09:29:30 |
| Eccentricity: | 0.0008436 |
| inclination: | 49.9795° |
| perigee height: | 611 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 144.6066° |
| argument of perigee: | 183.3104° |
| revolutions per day: | 14.84073834 |
| mean anomaly at epoch: | 176.7780° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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