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 29713U 26109.20102510 +.00000000 +00000-0 +10860-3 0 00002
2 29713 98.0238 139.8514 0018947 301.3883 58.5485 14.98144671 00
| Epoch (UTC): | 19 April 2026 04:49:28 |
| Eccentricity: | 0.0018947 |
| inclination: | 98.0238° |
| perigee height: | 559 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 139.8514° |
| argument of perigee: | 301.3883° |
| revolutions per day: | 14.98144671 |
| mean anomaly at epoch: | 58.5485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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