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 53577U 26145.49471955 +.00000000 +00000-0 +11747-3 0 00005
2 53577 53.2124 69.0770 0001464 87.0499 273.0660 15.08835868 03
| Epoch (UTC): | 25 May 2026 11:52:23 |
| Eccentricity: | 0.0001464 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 69.0770° |
| argument of perigee: | 87.0499° |
| revolutions per day: | 15.08835868 |
| mean anomaly at epoch: | 273.0660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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