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 52599U 26145.12262353 +.00000000 +00000-0 +96930-4 0 00006
2 52599 53.2148 296.1044 0001239 92.3013 267.8121 15.08834650 01
| Epoch (UTC): | 25 May 2026 02:56:34 |
| Eccentricity: | 0.0001239 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 296.1044° |
| argument of perigee: | 92.3013° |
| revolutions per day: | 15.08834650 |
| mean anomaly at epoch: | 267.8121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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