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 26158.72002718 +.00000000 +00000-0 +10137-3 0 00002
2 28230 89.8515 50.3759 0002306 75.8031 284.3451 14.83270305 07
| Epoch (UTC): | 07 June 2026 17:16:50 |
| Eccentricity: | 0.0002306 |
| inclination: | 89.8515° |
| perigee height: | 617 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 50.3759° |
| argument of perigee: | 75.8031° |
| revolutions per day: | 14.83270305 |
| mean anomaly at epoch: | 284.3451° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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