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 04139U 26020.95035333 +.00000000 +00000-0 +22103-3 0 00002
2 04139 74.0295 197.0951 0005776 218.1587 141.9174 14.66385102 08
| Epoch (UTC): | 20 January 2026 22:48:30 |
| Eccentricity: | 0.0005776 |
| inclination: | 74.0295° |
| perigee height: | 669 km |
| apogee height: | 677 km |
| right ascension of ascending node: | 197.0951° |
| argument of perigee: | 218.1587° |
| revolutions per day: | 14.66385102 |
| mean anomaly at epoch: | 141.9174° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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