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 26150.71512682 +.00000000 +00000-0 +22478-3 0 00003
2 33499 98.1195 72.8808 0007800 358.1688 1.9495 14.83072924 08
| Epoch (UTC): | 30 May 2026 17:09:46 |
| Eccentricity: | 0.0007800 |
| inclination: | 98.1195° |
| perigee height: | 614 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 72.8808° |
| argument of perigee: | 358.1688° |
| revolutions per day: | 14.83072924 |
| mean anomaly at epoch: | 1.9495° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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