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 39533U 26145.24987852 +.00000000 +00000-0 +00000-0 0 00009
2 39533 53.6506 150.2551 0084167 230.8699 128.4053 2.00558342 04
| Epoch (UTC): | 25 May 2026 05:59:49 |
| Eccentricity: | 0.0084167 |
| inclination: | 53.6506° |
| perigee height: | 19959 km |
| apogee height: | 20406 km |
| right ascension of ascending node: | 150.2551° |
| argument of perigee: | 230.8699° |
| revolutions per day: | 2.00558342 |
| mean anomaly at epoch: | 128.4053° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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