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 26067.74828543 +.00000000 +00000-0 +77806-4 0 00009
2 18959 82.5399 170.5296 0017382 61.7882 298.5087 14.85674823 00
| Epoch (UTC): | 08 March 2026 17:57:31 |
| Eccentricity: | 0.0017382 |
| inclination: | 82.5399° |
| perigee height: | 599 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 170.5296° |
| argument of perigee: | 61.7882° |
| revolutions per day: | 14.85674823 |
| mean anomaly at epoch: | 298.5087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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