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 28647U 26106.22446024 +.00000000 +00000-0 +24216-3 0 00007
2 28647 56.9952 85.0328 0064087 86.7579 274.0805 15.44107977 09
| Epoch (UTC): | 16 April 2026 05:23:13 |
| Eccentricity: | 0.0064087 |
| inclination: | 56.9952° |
| perigee height: | 390 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 85.0328° |
| argument of perigee: | 86.7579° |
| revolutions per day: | 15.44107977 |
| mean anomaly at epoch: | 274.0805° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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