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 26073.59718053 +.00000000 +00000-0 +12759-3 0 00008
2 29092 97.7550 96.7210 0001524 93.8084 266.3307 14.87597186 09
| Epoch (UTC): | 14 March 2026 14:19:56 |
| Eccentricity: | 0.0001524 |
| inclination: | 97.7550° |
| perigee height: | 604 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 96.7210° |
| argument of perigee: | 93.8084° |
| revolutions per day: | 14.87597186 |
| mean anomaly at epoch: | 266.3307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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