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 23657U 26074.24693041 +.00000000 +00000-0 +16129-3 0 00006
2 23657 82.5235 131.5141 0017007 279.4186 80.5112 14.94387516 03
| Epoch (UTC): | 15 March 2026 05:55:34 |
| Eccentricity: | 0.0017007 |
| inclination: | 82.5235° |
| perigee height: | 572 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 131.5141° |
| argument of perigee: | 279.4186° |
| revolutions per day: | 14.94387516 |
| mean anomaly at epoch: | 80.5112° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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