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 00016U 26100.50156049 +.00000000 +00000-0 +86078-4 0 00002
2 00016 34.2616 140.7504 2018990 194.7322 158.4683 10.49583577 03
| Epoch (UTC): | 10 April 2026 12:02:14 |
| Eccentricity: | 0.2018990 |
| inclination: | 34.2616° |
| perigee height: | 654 km |
| apogee height: | 4213 km |
| right ascension of ascending node: | 140.7504° |
| argument of perigee: | 194.7322° |
| revolutions per day: | 10.49583577 |
| mean anomaly at epoch: | 158.4683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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