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 33785U 26019.37637184 +.00000000 +00000-0 +22074-2 0 00003
2 33785 73.8675 346.0813 0023171 281.7491 196.1685 14.71482723 00
| Epoch (UTC): | 19 January 2026 09:01:58 |
| Eccentricity: | 0.0023171 |
| inclination: | 73.8675° |
| perigee height: | 640 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 346.0813° |
| argument of perigee: | 281.7491° |
| revolutions per day: | 14.71482723 |
| mean anomaly at epoch: | 196.1685° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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