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 40071U 26160.16841250 +.00000000 +00000-0 +20494-3 0 00009
2 40071 98.3863 121.3839 0006064 307.0113 53.0547 14.89961306 00
| Epoch (UTC): | 09 June 2026 04:02:30 |
| Eccentricity: | 0.0006064 |
| inclination: | 98.3863° |
| perigee height: | 594 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 121.3839° |
| argument of perigee: | 307.0113° |
| revolutions per day: | 14.89961306 |
| mean anomaly at epoch: | 53.0547° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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