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 26106.56224251 +.00000000 +00000-0 +00000-0 0 00009
2 03029 3.0207 79.0716 0015132 30.1511 192.6137 1.00271949 03
| Epoch (UTC): | 16 April 2026 13:29:37 |
| Eccentricity: | 0.0015132 |
| inclination: | 3.0207° |
| perigee height: | 35723 km |
| apogee height: | 35850 km |
| right ascension of ascending node: | 79.0716° |
| argument of perigee: | 30.1511° |
| revolutions per day: | 1.00271949 |
| mean anomaly at epoch: | 192.6137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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