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 26156.57671545 +.00000000 +00000-0 +00000-0 0 00007
2 03029 3.1493 78.5133 0015640 32.8808 244.9954 1.00272011 09
| Epoch (UTC): | 05 June 2026 13:50:28 |
| Eccentricity: | 0.0015640 |
| inclination: | 3.1493° |
| perigee height: | 35721 km |
| apogee height: | 35852 km |
| right ascension of ascending node: | 78.5133° |
| argument of perigee: | 32.8808° |
| revolutions per day: | 1.00272011 |
| mean anomaly at epoch: | 244.9954° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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