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 20433U 26159.26272228 +.00000000 +00000-0 +68805-4 0 00000
2 20433 74.0359 94.0212 0039432 144.9804 326.9757 14.37540617 08
| Epoch (UTC): | 08 June 2026 06:18:19 |
| Eccentricity: | 0.0039432 |
| inclination: | 74.0359° |
| perigee height: | 738 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 94.0212° |
| argument of perigee: | 144.9804° |
| revolutions per day: | 14.37540617 |
| mean anomaly at epoch: | 326.9757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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