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 26065.05460633 +.00000000 +00000-0 +12892-3 0 00006
2 29092 97.7557 88.3707 0001468 93.5236 266.6148 14.87575194 08
| Epoch (UTC): | 06 March 2026 01:18:37 |
| Eccentricity: | 0.0001468 |
| inclination: | 97.7557° |
| perigee height: | 604 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 88.3707° |
| argument of perigee: | 93.5236° |
| revolutions per day: | 14.87575194 |
| mean anomaly at epoch: | 266.6148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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