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 26075.18567536 +.00000000 +00000-0 +12687-3 0 00008
2 04139 74.0289 92.5128 0003531 89.2108 270.9465 14.66484989 08
| Epoch (UTC): | 16 March 2026 04:27:22 |
| Eccentricity: | 0.0003531 |
| inclination: | 74.0289° |
| perigee height: | 670 km |
| apogee height: | 675 km |
| right ascension of ascending node: | 92.5128° |
| argument of perigee: | 89.2108° |
| revolutions per day: | 14.66484989 |
| mean anomaly at epoch: | 270.9465° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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