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 53606U 26145.26476733 +.00000000 +00000-0 +25822-4 0 00002
2 53606 53.2149 250.4734 0001073 87.2471 272.8644 15.08832867 02
| Epoch (UTC): | 25 May 2026 06:21:15 |
| Eccentricity: | 0.0001073 |
| inclination: | 53.2149° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 250.4734° |
| argument of perigee: | 87.2471° |
| revolutions per day: | 15.08832867 |
| mean anomaly at epoch: | 272.8644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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