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 33321U 26145.60405291 +.00000000 +00000-0 +15032-3 0 00004
2 33321 97.6516 135.5578 0034699 257.3684 102.3650 14.83273198 01
| Epoch (UTC): | 25 May 2026 14:29:50 |
| Eccentricity: | 0.0034699 |
| inclination: | 97.6516° |
| perigee height: | 595 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 135.5578° |
| argument of perigee: | 257.3684° |
| revolutions per day: | 14.83273198 |
| mean anomaly at epoch: | 102.3650° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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