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 26150.52862059 +.00000000 +00000-0 +20058-3 0 00004
2 33321 97.6505 140.2758 0034829 240.4105 119.3637 14.83284477 03
| Epoch (UTC): | 30 May 2026 12:41:12 |
| Eccentricity: | 0.0034829 |
| inclination: | 97.6505° |
| perigee height: | 595 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 140.2758° |
| argument of perigee: | 240.4105° |
| revolutions per day: | 14.83284477 |
| mean anomaly at epoch: | 119.3637° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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