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 57119U 26145.47796115 +.00000000 +00000-0 -15023-3 0 00009
2 57119 42.9998 208.1021 0001393 284.0068 76.0628 15.27554051 08
| Epoch (UTC): | 25 May 2026 11:28:15 |
| Eccentricity: | 0.0001393 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 208.1021° |
| argument of perigee: | 284.0068° |
| revolutions per day: | 15.27554051 |
| mean anomaly at epoch: | 76.0628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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