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 23659U 26022.19349464 +.00000000 +00000-0 +95230-4 0 00003
2 23659 82.5287 268.7275 0025738 34.9252 84.2654 14.80269066 07
| Epoch (UTC): | 22 January 2026 04:38:37 |
| Eccentricity: | 0.0025738 |
| inclination: | 82.5287° |
| perigee height: | 610 km |
| apogee height: | 647 km |
| right ascension of ascending node: | 268.7275° |
| argument of perigee: | 34.9252° |
| revolutions per day: | 14.80269066 |
| mean anomaly at epoch: | 84.2654° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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