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 26150.07289965 +.00000000 +00000-0 +11011-3 0 00002
2 29092 97.7466 171.4447 0001442 89.3983 270.7398 14.87716154 02
| Epoch (UTC): | 30 May 2026 01:44:58 |
| Eccentricity: | 0.0001442 |
| inclination: | 97.7466° |
| perigee height: | 604 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 171.4447° |
| argument of perigee: | 89.3983° |
| revolutions per day: | 14.87716154 |
| mean anomaly at epoch: | 270.7398° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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