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 57120U 26145.45480988 +.00000000 +00000-0 +47108-4 0 00006
2 57120 43.0018 207.9305 0000956 270.1209 89.9533 15.27578651 04
| Epoch (UTC): | 25 May 2026 10:54:55 |
| Eccentricity: | 0.0000956 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 207.9305° |
| argument of perigee: | 270.1209° |
| revolutions per day: | 15.27578651 |
| mean anomaly at epoch: | 89.9533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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