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 26104.23062002 +.00000000 +00000-0 +77838-3 0 00006
2 39485 82.4851 207.9873 0020469 248.7416 111.1478 12.42876062 09
| Epoch (UTC): | 14 April 2026 05:32:05 |
| Eccentricity: | 0.0020469 |
| inclination: | 82.4851° |
| perigee height: | 1478 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 207.9873° |
| argument of perigee: | 248.7416° |
| revolutions per day: | 12.42876062 |
| mean anomaly at epoch: | 111.1478° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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