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 54153U 26144.27366501 +.00000000 +00000-0 +00000-0 0 00008
2 54153 89.9543 96.6746 0007378 209.4053 150.5897 5.00435639 04
| Epoch (UTC): | 24 May 2026 06:34:04 |
| Eccentricity: | 0.0007378 |
| inclination: | 89.9543° |
| perigee height: | 8049 km |
| apogee height: | 8070 km |
| right ascension of ascending node: | 96.6746° |
| argument of perigee: | 209.4053° |
| revolutions per day: | 5.00435639 |
| mean anomaly at epoch: | 150.5897° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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