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 26140.51190911 +.00000000 +00000-0 +00000-0 0 00008
2 39120 4.4310 52.4828 0002211 1.1813 318.9945 1.00271466 04
| Epoch (UTC): | 20 May 2026 12:17:08 |
| Eccentricity: | 0.0002211 |
| inclination: | 4.4310° |
| perigee height: | 35777 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 52.4828° |
| argument of perigee: | 1.1813° |
| revolutions per day: | 1.00271466 |
| mean anomaly at epoch: | 318.9945° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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