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 43476U 18047A 26154.12509240 +.00002735 00000-0 +72578-4 0 08
2 43476 88.9921 199.8885 0012563 152.6432 299.1218 15.38163494447642
| Epoch (UTC): | 03 June 2026 03:00:07 |
| Eccentricity: | 0.0012563 |
| inclination: | 88.9921° |
| perigee height: | 443 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 199.8885° |
| argument of perigee: | 152.6432° |
| revolutions per day: | 15.38163494 |
| mean anomaly at epoch: | 299.1218° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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