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 28890U 26150.51153604 +.00000000 +00000-0 +62108-4 0 00000
2 28890 98.2882 283.6281 0014219 342.1968 17.8733 14.63520452 07
| Epoch (UTC): | 30 May 2026 12:16:36 |
| Eccentricity: | 0.0014219 |
| inclination: | 98.2882° |
| perigee height: | 672 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 283.6281° |
| argument of perigee: | 342.1968° |
| revolutions per day: | 14.63520452 |
| mean anomaly at epoch: | 17.8733° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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