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 39679U 26109.12408147 +.00000000 +00000-0 +21228-3 0 00000
2 39679 51.6046 139.8068 0093009 250.8460 108.2439 15.40530065 05
| Epoch (UTC): | 19 April 2026 02:58:40 |
| Eccentricity: | 0.0093009 |
| inclination: | 51.6046° |
| perigee height: | 381 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 139.8068° |
| argument of perigee: | 250.8460° |
| revolutions per day: | 15.40530065 |
| mean anomaly at epoch: | 108.2439° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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