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 39485U 26145.60653036 +.00000000 +00000-0 -47982-3 0 00003
2 39485 82.4829 182.2126 0022102 157.5008 202.7045 12.42876952 05
| Epoch (UTC): | 25 May 2026 14:33:24 |
| Eccentricity: | 0.0022102 |
| inclination: | 82.4829° |
| perigee height: | 1477 km |
| apogee height: | 1512 km |
| right ascension of ascending node: | 182.2126° |
| argument of perigee: | 157.5008° |
| revolutions per day: | 12.42876952 |
| mean anomaly at epoch: | 202.7045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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