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 26053.50865425 +.00000000 +00000-0 +00000-0 0 00008
2 03029 2.8829 79.7367 0014480 29.7270 120.7675 1.00271790 03
| Epoch (UTC): | 22 February 2026 12:12:27 |
| Eccentricity: | 0.0014480 |
| inclination: | 2.8829° |
| perigee height: | 35726 km |
| apogee height: | 35848 km |
| right ascension of ascending node: | 79.7367° |
| argument of perigee: | 29.7270° |
| revolutions per day: | 1.00271790 |
| mean anomaly at epoch: | 120.7675° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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