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 19460U 26138.44410367 +.00000000 +00000-0 +30037-4 0 00009
2 19460 84.9843 130.3654 0002871 164.2666 195.8618 14.34435536 05
| Epoch (UTC): | 18 May 2026 10:39:30 |
| Eccentricity: | 0.0002871 |
| inclination: | 84.9843° |
| perigee height: | 775 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 130.3654° |
| argument of perigee: | 164.2666° |
| revolutions per day: | 14.34435536 |
| mean anomaly at epoch: | 195.8618° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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