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 26145.62270818 +.00000000 +00000-0 +41910-3 0 00001
2 33408 97.8429 178.1622 0013036 90.4705 269.8021 15.16907300 04
| Epoch (UTC): | 25 May 2026 14:56:41 |
| Eccentricity: | 0.0013036 |
| inclination: | 97.8429° |
| perigee height: | 506 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 178.1622° |
| argument of perigee: | 90.4705° |
| revolutions per day: | 15.16907300 |
| mean anomaly at epoch: | 269.8021° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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