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 57752U 26145.25819920 +.00000000 +00000-0 +56094-4 0 00001
2 57752 43.0044 100.2551 0000959 282.3095 77.7649 15.27577019 03
| Epoch (UTC): | 25 May 2026 06:11:48 |
| Eccentricity: | 0.0000959 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.2551° |
| argument of perigee: | 282.3095° |
| revolutions per day: | 15.27577019 |
| mean anomaly at epoch: | 77.7649° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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