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 26069.76881638 +.00000000 +00000-0 +65042-4 0 00006
2 18959 82.5397 168.6354 0017273 55.5463 304.7383 14.85676994 06
| Epoch (UTC): | 10 March 2026 18:27:05 |
| Eccentricity: | 0.0017273 |
| inclination: | 82.5397° |
| perigee height: | 599 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 168.6354° |
| argument of perigee: | 55.5463° |
| revolutions per day: | 14.85676994 |
| mean anomaly at epoch: | 304.7383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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