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 43010U 26145.59538685 +.00000000 +00000-0 -63224-4 0 00000
2 43010 99.0117 119.6113 0002519 99.6383 260.5077 14.19733360 08
| Epoch (UTC): | 25 May 2026 14:17:21 |
| Eccentricity: | 0.0002519 |
| inclination: | 99.0117° |
| perigee height: | 824 km |
| apogee height: | 828 km |
| right ascension of ascending node: | 119.6113° |
| argument of perigee: | 99.6383° |
| revolutions per day: | 14.19733360 |
| mean anomaly at epoch: | 260.5077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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