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 15071U 26146.28165226 +.00000000 +00000-0 +27941-3 0 00004
2 15071 95.8858 20.3852 0005855 61.9302 298.2525 15.13947311 01
| Epoch (UTC): | 26 May 2026 06:45:34 |
| Eccentricity: | 0.0005855 |
| inclination: | 95.8858° |
| perigee height: | 520 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 20.3852° |
| argument of perigee: | 61.9302° |
| revolutions per day: | 15.13947311 |
| mean anomaly at epoch: | 298.2525° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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