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 53411U 26145.22426463 +.00000000 +00000-0 +77402-4 0 00008
2 53411 53.2143 130.5430 0000956 69.3752 290.7343 15.08841191 08
| Epoch (UTC): | 25 May 2026 05:22:56 |
| Eccentricity: | 0.0000956 |
| inclination: | 53.2143° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 130.5430° |
| argument of perigee: | 69.3752° |
| revolutions per day: | 15.08841191 |
| mean anomaly at epoch: | 290.7343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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