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 23751U 26150.51113676 +.00000000 +00000-0 +71786-4 0 00008
2 23751 99.0217 169.1326 0001178 85.0832 275.0480 14.23564133 07
| Epoch (UTC): | 30 May 2026 12:16:02 |
| Eccentricity: | 0.0001178 |
| inclination: | 99.0217° |
| perigee height: | 812 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 169.1326° |
| argument of perigee: | 85.0832° |
| revolutions per day: | 14.23564133 |
| mean anomaly at epoch: | 275.0480° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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