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 03428U 26108.59113134 +.00000000 +00000-0 +00000-0 0 00004
2 03428 1.8828 49.0204 0080764 284.3244 144.5944 1.01561428 06
| Epoch (UTC): | 18 April 2026 14:11:13 |
| Eccentricity: | 0.0080764 |
| inclination: | 1.8828° |
| perigee height: | 35091 km |
| apogee height: | 35767 km |
| right ascension of ascending node: | 49.0204° |
| argument of perigee: | 284.3244° |
| revolutions per day: | 1.01561428 |
| mean anomaly at epoch: | 144.5944° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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