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 26040.19929936 +.00000000 +00000-0 +57001-3 0 00006
2 28647 56.9994 9.0489 0058724 326.0889 33.6416 15.41415492 02
| Epoch (UTC): | 09 February 2026 04:46:59 |
| Eccentricity: | 0.0058724 |
| inclination: | 56.9994° |
| perigee height: | 402 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 9.0489° |
| argument of perigee: | 326.0889° |
| revolutions per day: | 15.41415492 |
| mean anomaly at epoch: | 33.6416° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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