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 26032.57659291 +.00000000 +00000-0 +29322-3 0 00004
2 33412 97.8450 248.8367 0016499 11.7476 348.4132 15.05906143 00
| Epoch (UTC): | 01 February 2026 13:50:17 |
| Eccentricity: | 0.0016499 |
| inclination: | 97.8450° |
| perigee height: | 537 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 248.8367° |
| argument of perigee: | 11.7476° |
| revolutions per day: | 15.05906143 |
| mean anomaly at epoch: | 348.4132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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