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 23323U 26150.15142053 +.00000000 +00000-0 +72236-4 0 00005
2 23323 98.8947 200.4564 0001099 99.2190 260.9112 14.24662349 02
| Epoch (UTC): | 30 May 2026 03:38:02 |
| Eccentricity: | 0.0001099 |
| inclination: | 98.8947° |
| perigee height: | 809 km |
| apogee height: | 810 km |
| right ascension of ascending node: | 200.4564° |
| argument of perigee: | 99.2190° |
| revolutions per day: | 14.24662349 |
| mean anomaly at epoch: | 260.9112° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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