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 23317U 26032.22218270 +.00000000 +00000-0 +18876-3 0 00009
2 23317 82.5327 24.8282 0017004 18.1783 342.0043 14.96666482 09
| Epoch (UTC): | 01 February 2026 05:19:56 |
| Eccentricity: | 0.0017004 |
| inclination: | 82.5327° |
| perigee height: | 565 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 24.8282° |
| argument of perigee: | 18.1783° |
| revolutions per day: | 14.96666482 |
| mean anomaly at epoch: | 342.0043° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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