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 33412U 26067.59029255 +.00000000 +00000-0 +34463-3 0 00007
2 33412 97.8418 284.4590 0014419 245.3754 114.5971 15.06237155 06
| Epoch (UTC): | 08 March 2026 14:10:01 |
| Eccentricity: | 0.0014419 |
| inclination: | 97.8418° |
| perigee height: | 538 km |
| apogee height: | 558 km |
| right ascension of ascending node: | 284.4590° |
| argument of perigee: | 245.3754° |
| revolutions per day: | 15.06237155 |
| mean anomaly at epoch: | 114.5971° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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