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 19420U 26106.67758537 +.00000000 +00000-0 +77701-4 0 00008
2 19420 90.0471 21.0759 0092403 243.7860 182.9078 13.42603651 07
| Epoch (UTC): | 16 April 2026 16:15:43 |
| Eccentricity: | 0.0092403 |
| inclination: | 90.0471° |
| perigee height: | 1031 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 21.0759° |
| argument of perigee: | 243.7860° |
| revolutions per day: | 13.42603651 |
| mean anomaly at epoch: | 182.9078° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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