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 33408U 26150.57000355 +.00000000 +00000-0 +52837-3 0 00008
2 33408 97.8415 183.2800 0012849 75.7482 284.5177 15.16975418 04
| Epoch (UTC): | 30 May 2026 13:40:48 |
| Eccentricity: | 0.0012849 |
| inclination: | 97.8415° |
| perigee height: | 506 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 183.2800° |
| argument of perigee: | 75.7482° |
| revolutions per day: | 15.16975418 |
| mean anomaly at epoch: | 284.5177° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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