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 26064.20298920 +.00000000 +00000-0 +22283-3 0 00006
2 23657 82.5253 141.0787 0017407 315.7424 44.2404 14.94344343 00
| Epoch (UTC): | 05 March 2026 04:52:18 |
| Eccentricity: | 0.0017407 |
| inclination: | 82.5253° |
| perigee height: | 572 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 141.0787° |
| argument of perigee: | 315.7424° |
| revolutions per day: | 14.94344343 |
| mean anomaly at epoch: | 44.2404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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