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 60733U 26145.64207069 +.00000000 +00000-0 +27109-4 0 00007
2 60733 53.1614 270.9097 0001120 80.7555 279.3573 15.30195861 04
| Epoch (UTC): | 25 May 2026 15:24:34 |
| Eccentricity: | 0.0001120 |
| inclination: | 53.1614° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 270.9097° |
| argument of perigee: | 80.7555° |
| revolutions per day: | 15.30195861 |
| mean anomaly at epoch: | 279.3573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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