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 53026U 26145.16909205 +.00000000 +00000-0 -38630-4 0 00004
2 53026 53.2127 100.6841 0001518 67.1165 292.9987 15.08841705 04
| Epoch (UTC): | 25 May 2026 04:03:29 |
| Eccentricity: | 0.0001518 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 100.6841° |
| argument of perigee: | 67.1165° |
| revolutions per day: | 15.08841705 |
| mean anomaly at epoch: | 292.9987° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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