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 26146.24915253 +.00000000 +00000-0 +50805-4 0 00005
2 29522 98.7381 153.2683 0011182 115.6362 244.5968 14.14988885 07
| Epoch (UTC): | 26 May 2026 05:58:46 |
| Eccentricity: | 0.0011182 |
| inclination: | 98.7381° |
| perigee height: | 834 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 153.2683° |
| argument of perigee: | 115.6362° |
| revolutions per day: | 14.14988885 |
| mean anomaly at epoch: | 244.5968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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