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 26104.19978108 +.00000000 +00000-0 +00000-0 0 00003
2 03029 3.0146 79.0984 0015075 30.1364 59.7848 1.00271919 03
| Epoch (UTC): | 14 April 2026 04:47:41 |
| Eccentricity: | 0.0015075 |
| inclination: | 3.0146° |
| perigee height: | 35723 km |
| apogee height: | 35850 km |
| right ascension of ascending node: | 79.0984° |
| argument of perigee: | 30.1364° |
| revolutions per day: | 1.00271919 |
| mean anomaly at epoch: | 59.7848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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