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 29050U 26088.19041110 +.00000000 +00000-0 +29493-3 0 00000
2 29050 72.0117 125.6067 0041331 71.6214 288.9431 14.66740963 07
| Epoch (UTC): | 29 March 2026 04:34:11 |
| Eccentricity: | 0.0041331 |
| inclination: | 72.0117° |
| perigee height: | 642 km |
| apogee height: | 701 km |
| right ascension of ascending node: | 125.6067° |
| argument of perigee: | 71.6214° |
| revolutions per day: | 14.66740963 |
| mean anomaly at epoch: | 288.9431° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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