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 26145.52002073 +.00000000 +00000-0 +14734-3 0 00000
2 33499 98.1194 67.6038 0008224 14.5209 345.6239 14.83053917 02
| Epoch (UTC): | 25 May 2026 12:28:49 |
| Eccentricity: | 0.0008224 |
| inclination: | 98.1194° |
| perigee height: | 614 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 67.6038° |
| argument of perigee: | 14.5209° |
| revolutions per day: | 14.83053917 |
| mean anomaly at epoch: | 345.6239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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