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 53406U 26145.34202763 +.00000000 +00000-0 +58541-4 0 00003
2 53406 53.2126 130.0159 0000977 80.0728 280.0374 15.08838503 01
| Epoch (UTC): | 25 May 2026 08:12:31 |
| Eccentricity: | 0.0000977 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 130.0159° |
| argument of perigee: | 80.0728° |
| revolutions per day: | 15.08838503 |
| mean anomaly at epoch: | 280.0374° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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