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 39211U 26020.70567316 +.00000000 +00000-0 +87890-3 0 00009
2 39211 97.9665 292.3543 0072909 78.0580 282.8823 15.33949852 05
| Epoch (UTC): | 20 January 2026 16:56:10 |
| Eccentricity: | 0.0072909 |
| inclination: | 97.9665° |
| perigee height: | 414 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 292.3543° |
| argument of perigee: | 78.0580° |
| revolutions per day: | 15.33949852 |
| mean anomaly at epoch: | 282.8823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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