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 26019.24449476 +.00000000 +00000-0 +41736-3 0 00002
2 28647 56.9988 98.9222 0058480 282.8609 76.5915 15.40325678 00
| Epoch (UTC): | 19 January 2026 05:52:04 |
| Eccentricity: | 0.0058480 |
| inclination: | 56.9988° |
| perigee height: | 405 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 98.9222° |
| argument of perigee: | 282.8609° |
| revolutions per day: | 15.40325678 |
| mean anomaly at epoch: | 76.5915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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