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 29522U 26140.59222171 +.00000000 +00000-0 +24123-4 0 00001
2 29522 98.7383 147.7269 0010988 130.2713 229.9423 14.14987859 06
| Epoch (UTC): | 20 May 2026 14:12:47 |
| Eccentricity: | 0.0010988 |
| inclination: | 98.7383° |
| perigee height: | 834 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 147.7269° |
| argument of perigee: | 130.2713° |
| revolutions per day: | 14.14987859 |
| mean anomaly at epoch: | 229.9423° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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