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 29228U 26071.77551628 +.00000000 +00000-0 +22706-3 0 00003
2 29228 69.9325 229.0399 0001570 159.9148 200.2081 15.12769237 09
| Epoch (UTC): | 12 March 2026 18:36:44 |
| Eccentricity: | 0.0001570 |
| inclination: | 69.9325° |
| perigee height: | 527 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 229.0399° |
| argument of perigee: | 159.9148° |
| revolutions per day: | 15.12769237 |
| mean anomaly at epoch: | 200.2081° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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