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 33446U 26032.41804275 +.00000000 +00000-0 +17474-3 0 00003
2 33446 97.9224 327.0380 0015027 147.8408 212.3725 14.82865051 07
| Epoch (UTC): | 01 February 2026 10:01:58 |
| Eccentricity: | 0.0015027 |
| inclination: | 97.9224° |
| perigee height: | 610 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 327.0380° |
| argument of perigee: | 147.8408° |
| revolutions per day: | 14.82865051 |
| mean anomaly at epoch: | 212.3725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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