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 39092U 26110.33409389 +.00000000 +00000-0 +47477-4 0 00008
2 39092 98.4021 291.3017 0010066 54.3629 305.8494 14.36389031 05
| Epoch (UTC): | 20 April 2026 08:01:05 |
| Eccentricity: | 0.0010066 |
| inclination: | 98.4021° |
| perigee height: | 763 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 291.3017° |
| argument of perigee: | 54.3629° |
| revolutions per day: | 14.36389031 |
| mean anomaly at epoch: | 305.8494° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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