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 19876U 26150.28674521 +.00000000 +00000-0 +00000-0 0 00003
2 19876 14.8934 346.4734 0020496 209.1071 142.5738 0.97110538 08
| Epoch (UTC): | 30 May 2026 06:52:54 |
| Eccentricity: | 0.0020496 |
| inclination: | 14.8934° |
| perigee height: | 36608 km |
| apogee height: | 36785 km |
| right ascension of ascending node: | 346.4734° |
| argument of perigee: | 209.1071° |
| revolutions per day: | 0.97110538 |
| mean anomaly at epoch: | 142.5738° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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