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 33331U 26106.94222483 +.00000000 +00000-0 +55104-4 0 00004
2 33331 98.1255 181.6452 0002962 245.3396 114.7499 14.64667682 08
| Epoch (UTC): | 16 April 2026 22:36:48 |
| Eccentricity: | 0.0002962 |
| inclination: | 98.1255° |
| perigee height: | 676 km |
| apogee height: | 680 km |
| right ascension of ascending node: | 181.6452° |
| argument of perigee: | 245.3396° |
| revolutions per day: | 14.64667682 |
| mean anomaly at epoch: | 114.7499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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