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 15334U 26088.19437997 +.00000000 +00000-0 +20268-3 0 00003
2 15334 71.0015 147.6268 0002081 139.9538 220.1739 14.15646610 03
| Epoch (UTC): | 29 March 2026 04:39:54 |
| Eccentricity: | 0.0002081 |
| inclination: | 71.0015° |
| perigee height: | 839 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 147.6268° |
| argument of perigee: | 139.9538° |
| revolutions per day: | 14.15646610 |
| mean anomaly at epoch: | 220.1739° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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