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 53182U 26145.29372375 +.00000000 +00000-0 +27677-4 0 00001
2 53182 53.2135 155.2203 0000911 80.3770 279.7325 15.08843791 05
| Epoch (UTC): | 25 May 2026 07:02:57 |
| Eccentricity: | 0.0000911 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 155.2203° |
| argument of perigee: | 80.3770° |
| revolutions per day: | 15.08843791 |
| mean anomaly at epoch: | 279.7325° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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