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 29678U 26150.21637806 +.00000000 +00000-0 +19349-3 0 00001
2 29678 90.1038 36.9368 0185362 184.4080 175.5506 14.50351015 04
| Epoch (UTC): | 30 May 2026 05:11:35 |
| Eccentricity: | 0.0185362 |
| inclination: | 90.1038° |
| perigee height: | 593 km |
| apogee height: | 856 km |
| right ascension of ascending node: | 36.9368° |
| argument of perigee: | 184.4080° |
| revolutions per day: | 14.50351015 |
| mean anomaly at epoch: | 175.5506° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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