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 29092U 26070.57029803 +.00000000 +00000-0 +12792-3 0 00008
2 29092 97.7554 93.7623 0001485 94.6849 265.4537 14.87589497 03
| Epoch (UTC): | 11 March 2026 13:41:13 |
| Eccentricity: | 0.0001485 |
| inclination: | 97.7554° |
| perigee height: | 604 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 93.7623° |
| argument of perigee: | 94.6849° |
| revolutions per day: | 14.87589497 |
| mean anomaly at epoch: | 265.4537° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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