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 33499U 26073.25588436 +.00000000 +00000-0 +24389-3 0 00009
2 33499 98.1185 354.2207 0006632 232.8662 127.1946 14.82848926 03
| Epoch (UTC): | 14 March 2026 06:08:28 |
| Eccentricity: | 0.0006632 |
| inclination: | 98.1185° |
| perigee height: | 616 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 354.2207° |
| argument of perigee: | 232.8662° |
| revolutions per day: | 14.82848926 |
| mean anomaly at epoch: | 127.1946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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