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 23233U 26146.23101699 +.00000000 +00000-0 +31085-4 0 00007
2 23233 98.6702 197.0481 0010484 341.7381 18.3415 14.16069247 03
| Epoch (UTC): | 26 May 2026 05:32:39 |
| Eccentricity: | 0.0010484 |
| inclination: | 98.6702° |
| perigee height: | 831 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 197.0481° |
| argument of perigee: | 341.7381° |
| revolutions per day: | 14.16069247 |
| mean anomaly at epoch: | 18.3415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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