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 59588U 26138.54807567 +.00000000 +00000-0 +52508-3 0 00003
2 59588 97.1736 63.9710 0024658 359.2841 0.8285 13.92684198 07
| Epoch (UTC): | 18 May 2026 13:09:13 |
| Eccentricity: | 0.0024658 |
| inclination: | 97.1736° |
| perigee height: | 901 km |
| apogee height: | 937 km |
| right ascension of ascending node: | 63.9710° |
| argument of perigee: | 359.2841° |
| revolutions per day: | 13.92684198 |
| mean anomaly at epoch: | 0.8285° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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