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 28738U 26105.93203191 +.00000000 +00000-0 +31610-3 0 00007
2 28738 97.3545 122.5373 0003183 202.8220 157.2898 15.63613697 04
| Epoch (UTC): | 15 April 2026 22:22:07 |
| Eccentricity: | 0.0003183 |
| inclination: | 97.3545° |
| perigee height: | 375 km |
| apogee height: | 379 km |
| right ascension of ascending node: | 122.5373° |
| argument of perigee: | 202.8220° |
| revolutions per day: | 15.63613697 |
| mean anomaly at epoch: | 157.2898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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