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 53819U 26145.19941752 +.00000000 +00000-0 +41482-4 0 00008
2 53819 53.2149 320.5267 0001016 112.9232 247.1868 15.08846732 05
| Epoch (UTC): | 25 May 2026 04:47:09 |
| Eccentricity: | 0.0001016 |
| inclination: | 53.2149° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 320.5267° |
| argument of perigee: | 112.9232° |
| revolutions per day: | 15.08846732 |
| mean anomaly at epoch: | 247.1868° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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