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 57087U 26145.38302520 +.00000000 +00000-0 +87741-4 0 00002
2 57087 43.0063 22.6568 0001838 275.5633 84.5009 15.27580423 08
| Epoch (UTC): | 25 May 2026 09:11:33 |
| Eccentricity: | 0.0001838 |
| inclination: | 43.0063° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 22.6568° |
| argument of perigee: | 275.5633° |
| revolutions per day: | 15.27580423 |
| mean anomaly at epoch: | 84.5009° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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