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 46027U 26145.28410122 +.00000000 +00000-0 +12697-2 0 00007
2 46027 53.0622 140.3283 0003140 10.9459 349.1600 15.12390763 06
| Epoch (UTC): | 25 May 2026 06:49:06 |
| Eccentricity: | 0.0003140 |
| inclination: | 53.0622° |
| perigee height: | 527 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 140.3283° |
| argument of perigee: | 10.9459° |
| revolutions per day: | 15.12390763 |
| mean anomaly at epoch: | 349.1600° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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