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 52159U 26103.24326361 +.00000000 +00000-0 -38073-5 0 00001
2 52159 97.9790 186.4145 0001676 99.9668 260.1730 14.75008761 09
| Epoch (UTC): | 13 April 2026 05:50:17 |
| Eccentricity: | 0.0001676 |
| inclination: | 97.9790° |
| perigee height: | 644 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 186.4145° |
| argument of perigee: | 99.9668° |
| revolutions per day: | 14.75008761 |
| mean anomaly at epoch: | 260.1730° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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