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 38833U 26144.38504975 +.00000000 +00000-0 +00000-0 0 00006
2 38833 53.5811 144.5742 0179097 65.4338 296.4391 2.00567085 06
| Epoch (UTC): | 24 May 2026 09:14:28 |
| Eccentricity: | 0.0179097 |
| inclination: | 53.5811° |
| perigee height: | 19706 km |
| apogee height: | 20658 km |
| right ascension of ascending node: | 144.5742° |
| argument of perigee: | 65.4338° |
| revolutions per day: | 2.00567085 |
| mean anomaly at epoch: | 296.4391° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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