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 26145.60845682 +.00000000 +00000-0 +81571-4 0 00009
2 33331 98.1239 219.8254 0005344 123.9147 236.2565 14.64700022 06
| Epoch (UTC): | 25 May 2026 14:36:10 |
| Eccentricity: | 0.0005344 |
| inclination: | 98.1239° |
| perigee height: | 674 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 219.8254° |
| argument of perigee: | 123.9147° |
| revolutions per day: | 14.64700022 |
| mean anomaly at epoch: | 236.2565° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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