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 54756U 26145.52249345 +.00000000 +00000-0 +00000-0 0 00002
2 54756 0.0515 342.7093 0005927 77.7518 299.5977 5.00115198 04
| Epoch (UTC): | 25 May 2026 12:32:23 |
| Eccentricity: | 0.0005927 |
| inclination: | 0.0515° |
| perigee height: | 8057 km |
| apogee height: | 8074 km |
| right ascension of ascending node: | 342.7093° |
| argument of perigee: | 77.7518° |
| revolutions per day: | 5.00115198 |
| mean anomaly at epoch: | 299.5977° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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