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 06020U 26018.57577523 +.00000000 +00000-0 +31170-4 0 00005
2 06020 74.0214 70.7200 0019703 67.5870 39.9505 13.79145233 06
| Epoch (UTC): | 18 January 2026 13:49:06 |
| Eccentricity: | 0.0019703 |
| inclination: | 74.0214° |
| perigee height: | 952 km |
| apogee height: | 981 km |
| right ascension of ascending node: | 70.7200° |
| argument of perigee: | 67.5870° |
| revolutions per day: | 13.79145233 |
| mean anomaly at epoch: | 39.9505° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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