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 39620U 26140.18259421 +.00000000 +00000-0 +00000-0 0 00008
2 39620 65.3143 314.8875 0010944 329.1830 30.7466 2.13103163 00
| Epoch (UTC): | 20 May 2026 04:22:56 |
| Eccentricity: | 0.0010944 |
| inclination: | 65.3143° |
| perigee height: | 19102 km |
| apogee height: | 19158 km |
| right ascension of ascending node: | 314.8875° |
| argument of perigee: | 329.1830° |
| revolutions per day: | 2.13103163 |
| mean anomaly at epoch: | 30.7466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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