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 46504U 26144.97988448 +.00000000 +00000-0 +37556-3 0 00005
2 46504 97.8613 151.3712 0006918 58.4513 301.7408 15.42986053 01
| Epoch (UTC): | 24 May 2026 23:31:02 |
| Eccentricity: | 0.0006918 |
| inclination: | 97.8613° |
| perigee height: | 433 km |
| apogee height: | 442 km |
| right ascension of ascending node: | 151.3712° |
| argument of perigee: | 58.4513° |
| revolutions per day: | 15.42986053 |
| mean anomaly at epoch: | 301.7408° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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