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 39985U 26082.48507615 +.00000000 +00000-0 +11384-2 0 00000
2 39985 82.5212 154.0620 0011652 122.4348 237.7957 14.12750109 03
| Epoch (UTC): | 23 March 2026 11:38:30 |
| Eccentricity: | 0.0011652 |
| inclination: | 82.5212° |
| perigee height: | 842 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 154.0620° |
| argument of perigee: | 122.4348° |
| revolutions per day: | 14.12750109 |
| mean anomaly at epoch: | 237.7957° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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