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 57112U 26145.53434963 +.00000000 +00000-0 +57127-4 0 00000
2 57112 43.0024 207.6712 0001121 276.4435 83.6289 15.27572429 02
| Epoch (UTC): | 25 May 2026 12:49:27 |
| Eccentricity: | 0.0001121 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 207.6712° |
| argument of perigee: | 276.4435° |
| revolutions per day: | 15.27572429 |
| mean anomaly at epoch: | 83.6289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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