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 26145.36424664 +.00000000 +00000-0 +10667-3 0 00009
2 33446 97.9304 79.0446 0015138 140.3657 219.8666 14.83149241 03
| Epoch (UTC): | 25 May 2026 08:44:30 |
| Eccentricity: | 0.0015138 |
| inclination: | 97.9304° |
| perigee height: | 609 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 79.0446° |
| argument of perigee: | 140.3657° |
| revolutions per day: | 14.83149241 |
| mean anomaly at epoch: | 219.8666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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