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 57121U 26145.56028552 +.00000000 +00000-0 -38239-4 0 00000
2 57121 43.0033 207.0137 0001805 297.7603 62.3065 15.26734597 00
| Epoch (UTC): | 25 May 2026 13:26:48 |
| Eccentricity: | 0.0001805 |
| inclination: | 43.0033° |
| perigee height: | 484 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 207.0137° |
| argument of perigee: | 297.7603° |
| revolutions per day: | 15.26734597 |
| mean anomaly at epoch: | 62.3065° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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