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 53784U 26145.38252363 +.00000000 +00000-0 -36551-4 0 00005
2 53784 53.2147 289.8706 0000478 68.9534 291.1509 15.08826094 05
| Epoch (UTC): | 25 May 2026 09:10:50 |
| Eccentricity: | 0.0000478 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 289.8706° |
| argument of perigee: | 68.9534° |
| revolutions per day: | 15.08826094 |
| mean anomaly at epoch: | 291.1509° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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