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 29052U 26104.09912682 +.00000000 +00000-0 +10082-3 0 00005
2 29052 72.0317 153.3059 0040812 272.1236 87.5229 14.31567689 07
| Epoch (UTC): | 14 April 2026 02:22:44 |
| Eccentricity: | 0.0040812 |
| inclination: | 72.0317° |
| perigee height: | 757 km |
| apogee height: | 816 km |
| right ascension of ascending node: | 153.3059° |
| argument of perigee: | 272.1236° |
| revolutions per day: | 14.31567689 |
| mean anomaly at epoch: | 87.5229° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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