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 29092U 26139.71502198 +.00000000 +00000-0 +48750-4 0 00007
2 29092 97.7477 161.3276 0001535 88.3717 271.7676 14.87699974 09
| Epoch (UTC): | 19 May 2026 17:09:37 |
| Eccentricity: | 0.0001535 |
| inclination: | 97.7477° |
| perigee height: | 604 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 161.3276° |
| argument of perigee: | 88.3717° |
| revolutions per day: | 14.87699974 |
| mean anomaly at epoch: | 271.7676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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