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 57983U 26145.64572211 +.00000000 +00000-0 +72987-4 0 00008
2 57983 42.9992 279.4095 0001522 274.6347 85.4330 15.27577934 01
| Epoch (UTC): | 25 May 2026 15:29:50 |
| Eccentricity: | 0.0001522 |
| inclination: | 42.9992° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 279.4095° |
| argument of perigee: | 274.6347° |
| revolutions per day: | 15.27577934 |
| mean anomaly at epoch: | 85.4330° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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