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 18959U 26064.31337352 +.00000000 +00000-0 +81104-4 0 00008
2 18959 82.5397 173.7495 0017513 72.2298 288.0828 14.85670420 04
| Epoch (UTC): | 05 March 2026 07:31:15 |
| Eccentricity: | 0.0017513 |
| inclination: | 82.5397° |
| perigee height: | 599 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 173.7495° |
| argument of perigee: | 72.2298° |
| revolutions per day: | 14.85670420 |
| mean anomaly at epoch: | 288.0828° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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