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 26067.81593419 +.00000000 +00000-0 +49616-3 0 00000
2 28647 56.9971 250.4007 0061657 18.4338 341.8931 15.42636767 02
| Epoch (UTC): | 08 March 2026 19:34:56 |
| Eccentricity: | 0.0061657 |
| inclination: | 56.9971° |
| perigee height: | 396 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 250.4007° |
| argument of perigee: | 18.4338° |
| revolutions per day: | 15.42636767 |
| mean anomaly at epoch: | 341.8931° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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