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 53781U 26145.11387516 +.00000000 +00000-0 +52877-4 0 00000
2 53781 53.2126 291.0358 0002330 79.5380 280.5875 15.08836060 05
| Epoch (UTC): | 25 May 2026 02:43:58 |
| Eccentricity: | 0.0002330 |
| inclination: | 53.2126° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 291.0358° |
| argument of perigee: | 79.5380° |
| revolutions per day: | 15.08836060 |
| mean anomaly at epoch: | 280.5875° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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