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 03029U 26088.16564697 +.00000000 +00000-0 +00000-0 0 00005
2 03029 2.9722 79.2933 0014907 29.7787 31.8493 1.00271881 08
| Epoch (UTC): | 29 March 2026 03:58:31 |
| Eccentricity: | 0.0014907 |
| inclination: | 2.9722° |
| perigee height: | 35724 km |
| apogee height: | 35849 km |
| right ascension of ascending node: | 79.2933° |
| argument of perigee: | 29.7787° |
| revolutions per day: | 1.00271881 |
| mean anomaly at epoch: | 31.8493° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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