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 39162U 26088.16147564 +.00000000 +00000-0 +42905-3 0 00005
2 39162 98.7968 59.4820 0081907 261.9951 97.1946 14.57243863 05
| Epoch (UTC): | 29 March 2026 03:52:31 |
| Eccentricity: | 0.0081907 |
| inclination: | 98.7968° |
| perigee height: | 644 km |
| apogee height: | 760 km |
| right ascension of ascending node: | 59.4820° |
| argument of perigee: | 261.9951° |
| revolutions per day: | 14.57243863 |
| mean anomaly at epoch: | 97.1946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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