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 26071.50187219 +.00000000 +00000-0 +14053-3 0 00005
2 04139 74.0292 99.6181 0003554 100.3451 259.8119 14.66479703 00
| Epoch (UTC): | 12 March 2026 12:02:41 |
| Eccentricity: | 0.0003554 |
| inclination: | 74.0292° |
| perigee height: | 670 km |
| apogee height: | 675 km |
| right ascension of ascending node: | 99.6181° |
| argument of perigee: | 100.3451° |
| revolutions per day: | 14.66479703 |
| mean anomaly at epoch: | 259.8119° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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