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 26017.88030286 +.00000000 +00000-0 +91945-4 0 00003
2 04139 74.0294 203.0149 0005898 223.8376 136.2326 14.66376735 06
| Epoch (UTC): | 17 January 2026 21:07:38 |
| Eccentricity: | 0.0005898 |
| inclination: | 74.0294° |
| perigee height: | 669 km |
| apogee height: | 677 km |
| right ascension of ascending node: | 203.0149° |
| argument of perigee: | 223.8376° |
| revolutions per day: | 14.66376735 |
| mean anomaly at epoch: | 136.2326° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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