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 10142U 26088.23784897 +.00000000 +00000-0 +77601-4 0 00008
2 10142 82.9678 156.0858 0043123 72.9781 348.2290 13.78902787 00
| Epoch (UTC): | 29 March 2026 05:42:30 |
| Eccentricity: | 0.0043123 |
| inclination: | 82.9678° |
| perigee height: | 936 km |
| apogee height: | 999 km |
| right ascension of ascending node: | 156.0858° |
| argument of perigee: | 72.9781° |
| revolutions per day: | 13.78902787 |
| mean anomaly at epoch: | 348.2290° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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