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 20439U 26039.08293257 +.00000000 +00000-0 +76000-4 0 00004
2 20439 98.8691 71.6360 0009594 248.3187 173.6577 14.33889619 02
| Epoch (UTC): | 08 February 2026 01:59:25 |
| Eccentricity: | 0.0009594 |
| inclination: | 98.8691° |
| perigee height: | 772 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 71.6360° |
| argument of perigee: | 248.3187° |
| revolutions per day: | 14.33889619 |
| mean anomaly at epoch: | 173.6577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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