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 26020.98757229 +.00000000 +00000-0 +35808-3 0 00002
2 29228 69.9346 0.3866 0005208 221.8589 138.2180 15.12416745 04
| Epoch (UTC): | 20 January 2026 23:42:06 |
| Eccentricity: | 0.0005208 |
| inclination: | 69.9346° |
| perigee height: | 525 km |
| apogee height: | 532 km |
| right ascension of ascending node: | 0.3866° |
| argument of perigee: | 221.8589° |
| revolutions per day: | 15.12416745 |
| mean anomaly at epoch: | 138.2180° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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