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 29656U 26152.16086497 +.00000000 +00000-0 +00000-0 0 00008
2 29656 11.5310 39.4037 0001839 3.7091 186.6915 0.99005142 04
| Epoch (UTC): | 01 June 2026 03:51:38 |
| Eccentricity: | 0.0001839 |
| inclination: | 11.5310° |
| perigee height: | 36138 km |
| apogee height: | 36153 km |
| right ascension of ascending node: | 39.4037° |
| argument of perigee: | 3.7091° |
| revolutions per day: | 0.99005142 |
| mean anomaly at epoch: | 186.6915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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