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 00029U 26139.75379916 +.00000000 +00000-0 +41851-4 0 00005
2 00029 48.3765 159.7713 0021741 147.7117 212.5132 14.78735999 00
| Epoch (UTC): | 19 May 2026 18:05:28 |
| Eccentricity: | 0.0021741 |
| inclination: | 48.3765° |
| perigee height: | 618 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 159.7713° |
| argument of perigee: | 147.7117° |
| revolutions per day: | 14.78735999 |
| mean anomaly at epoch: | 212.5132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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