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 26069.52352743 +.00000000 +00000-0 +14102-3 0 00005
2 04139 74.0295 103.4339 0003565 106.1228 254.0334 14.66476522 02
| Epoch (UTC): | 10 March 2026 12:33:52 |
| Eccentricity: | 0.0003565 |
| inclination: | 74.0295° |
| perigee height: | 670 km |
| apogee height: | 675 km |
| right ascension of ascending node: | 103.4339° |
| argument of perigee: | 106.1228° |
| revolutions per day: | 14.66476522 |
| mean anomaly at epoch: | 254.0334° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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