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 26133.44248875 +.00000000 +00000-0 +00000-0 0 00004
2 03029 3.0904 78.7682 0015464 31.3409 175.1328 1.00272017 07
| Epoch (UTC): | 13 May 2026 10:37:11 |
| Eccentricity: | 0.0015464 |
| inclination: | 3.0904° |
| perigee height: | 35721 km |
| apogee height: | 35852 km |
| right ascension of ascending node: | 78.7682° |
| argument of perigee: | 31.3409° |
| revolutions per day: | 1.00272017 |
| mean anomaly at epoch: | 175.1328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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