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 29049U 26106.57666611 +.00000000 +00000-0 +11199-3 0 00004
2 29049 72.0185 169.9211 0035266 312.1633 47.6510 14.31358817 03
| Epoch (UTC): | 16 April 2026 13:50:23 |
| Eccentricity: | 0.0035266 |
| inclination: | 72.0185° |
| perigee height: | 762 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 169.9211° |
| argument of perigee: | 312.1633° |
| revolutions per day: | 14.31358817 |
| mean anomaly at epoch: | 47.6510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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