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 53633U 26145.51959334 +.00000000 +00000-0 +46203-4 0 00009
2 53633 53.2129 239.2413 0001153 87.3472 272.7652 15.08836830 02
| Epoch (UTC): | 25 May 2026 12:28:12 |
| Eccentricity: | 0.0001153 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 239.2413° |
| argument of perigee: | 87.3472° |
| revolutions per day: | 15.08836830 |
| mean anomaly at epoch: | 272.7652° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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