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 57907U 26145.53541990 +.00000000 +00000-0 +18703-3 0 00007
2 57907 43.0042 240.6633 0001904 275.5535 84.5099 15.27591012 01
| Epoch (UTC): | 25 May 2026 12:51:00 |
| Eccentricity: | 0.0001904 |
| inclination: | 43.0042° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 240.6633° |
| argument of perigee: | 275.5535° |
| revolutions per day: | 15.27591012 |
| mean anomaly at epoch: | 84.5099° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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