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 39417U 26160.14189493 +.00000000 +00000-0 +23503-3 0 00007
2 39417 97.8092 122.4351 0040054 275.9917 83.6743 15.01137906 06
| Epoch (UTC): | 09 June 2026 03:24:19 |
| Eccentricity: | 0.0040054 |
| inclination: | 97.8092° |
| perigee height: | 536 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 122.4351° |
| argument of perigee: | 275.9917° |
| revolutions per day: | 15.01137906 |
| mean anomaly at epoch: | 83.6743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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