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 39120U 26145.50257167 +.00000000 +00000-0 +00000-0 0 00009
2 39120 4.4415 52.4870 0002140 4.0799 317.6497 1.00271384 00
| Epoch (UTC): | 25 May 2026 12:03:42 |
| Eccentricity: | 0.0002140 |
| inclination: | 4.4415° |
| perigee height: | 35778 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 52.4870° |
| argument of perigee: | 4.0799° |
| revolutions per day: | 1.00271384 |
| mean anomaly at epoch: | 317.6497° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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