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 28230U 26161.62097997 +.00000000 +00000-0 +71129-4 0 00007
2 28230 89.8512 50.3215 0002207 77.1683 282.9789 14.83273107 00
| Epoch (UTC): | 10 June 2026 14:54:12 |
| Eccentricity: | 0.0002207 |
| inclination: | 89.8512° |
| perigee height: | 617 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 50.3215° |
| argument of perigee: | 77.1683° |
| revolutions per day: | 14.83273107 |
| mean anomaly at epoch: | 282.9789° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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