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 26149.28119385 +.00000000 +00000-0 +10748-3 0 00006
2 00029 48.3770 114.4940 0022122 188.9579 171.0942 14.78748104 09
| Epoch (UTC): | 29 May 2026 06:44:55 |
| Eccentricity: | 0.0022122 |
| inclination: | 48.3770° |
| perigee height: | 618 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 114.4940° |
| argument of perigee: | 188.9579° |
| revolutions per day: | 14.78748104 |
| mean anomaly at epoch: | 171.0942° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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