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 00733U 26074.94130932 +.00000000 +00000-0 +89334-4 0 00007
2 00733 99.1222 88.6195 0032059 239.3879 120.4141 14.34023947 07
| Epoch (UTC): | 15 March 2026 22:35:29 |
| Eccentricity: | 0.0032059 |
| inclination: | 99.1222° |
| perigee height: | 755 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 88.6195° |
| argument of perigee: | 239.3879° |
| revolutions per day: | 14.34023947 |
| mean anomaly at epoch: | 120.4141° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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