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 33051U 26142.96411174 +.00000000 +00000-0 +00000-0 0 00003
2 33051 0.7062 85.6067 0005039 310.6370 283.7829 1.00268620 02
| Epoch (UTC): | 22 May 2026 23:08:19 |
| Eccentricity: | 0.0005039 |
| inclination: | 0.7062° |
| perigee height: | 35766 km |
| apogee height: | 35809 km |
| right ascension of ascending node: | 85.6067° |
| argument of perigee: | 310.6370° |
| revolutions per day: | 1.00268620 |
| mean anomaly at epoch: | 283.7829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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