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 03230U 26021.51930368 +.00000000 +00000-0 +44773-3 0 00005
2 03230 74.0305 50.0493 0026075 246.0648 113.7809 15.02856472 09
| Epoch (UTC): | 21 January 2026 12:27:47 |
| Eccentricity: | 0.0026075 |
| inclination: | 74.0305° |
| perigee height: | 540 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 50.0493° |
| argument of perigee: | 246.0648° |
| revolutions per day: | 15.02856472 |
| mean anomaly at epoch: | 113.7809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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