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 57227U 26145.49330236 +.00000000 +00000-0 +94922-4 0 00004
2 57227 43.0032 320.2031 0001754 265.3211 94.7440 15.27563301 06
| Epoch (UTC): | 25 May 2026 11:50:21 |
| Eccentricity: | 0.0001754 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 320.2031° |
| argument of perigee: | 265.3211° |
| revolutions per day: | 15.27563301 |
| mean anomaly at epoch: | 94.7440° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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