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 57433U 26145.50667154 +.00000000 +00000-0 -42609-5 0 00004
2 57433 43.0062 317.0070 0003020 268.0833 91.9673 15.27550185 06
| Epoch (UTC): | 25 May 2026 12:09:36 |
| Eccentricity: | 0.0003020 |
| inclination: | 43.0062° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 317.0070° |
| argument of perigee: | 268.0833° |
| revolutions per day: | 15.27550185 |
| mean anomaly at epoch: | 91.9673° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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