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 29506U 26150.55128713 +.00000000 +00000-0 +18484-3 0 00009
2 29506 97.7162 179.7186 0013683 113.2300 247.0367 15.01326186 08
| Epoch (UTC): | 30 May 2026 13:13:51 |
| Eccentricity: | 0.0013683 |
| inclination: | 97.7162° |
| perigee height: | 553 km |
| apogee height: | 572 km |
| right ascension of ascending node: | 179.7186° |
| argument of perigee: | 113.2300° |
| revolutions per day: | 15.01326186 |
| mean anomaly at epoch: | 247.0367° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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