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 26161.60341374 +.00000000 +00000-0 +46625-4 0 00004
2 19460 84.9858 116.8988 0004776 113.4262 246.7435 14.34442693 09
| Epoch (UTC): | 10 June 2026 14:28:54 |
| Eccentricity: | 0.0004776 |
| inclination: | 84.9858° |
| perigee height: | 774 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 116.8988° |
| argument of perigee: | 113.4262° |
| revolutions per day: | 14.34442693 |
| mean anomaly at epoch: | 246.7435° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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