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 57921U 26145.56608427 +.00000000 +00000-0 -27103-5 0 00002
2 57921 43.0029 251.1909 0001140 268.0016 92.0705 15.27567504 05
| Epoch (UTC): | 25 May 2026 13:35:09 |
| Eccentricity: | 0.0001140 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 251.1909° |
| argument of perigee: | 268.0016° |
| revolutions per day: | 15.27567504 |
| mean anomaly at epoch: | 92.0705° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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