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 26063.99237383 +.00000000 +00000-0 +45863-3 0 00000
2 28647 56.9957 266.8408 0061034 11.4390 348.8035 15.42455118 03
| Epoch (UTC): | 04 March 2026 23:49:01 |
| Eccentricity: | 0.0061034 |
| inclination: | 56.9957° |
| perigee height: | 397 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 266.8408° |
| argument of perigee: | 11.4390° |
| revolutions per day: | 15.42455118 |
| mean anomaly at epoch: | 348.8035° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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