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 57997U 26145.30593331 +.00000000 +00000-0 +62833-4 0 00001
2 57997 43.0070 354.3853 0001731 275.7543 84.3112 15.27587559 02
| Epoch (UTC): | 25 May 2026 07:20:32 |
| Eccentricity: | 0.0001731 |
| inclination: | 43.0070° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 354.3853° |
| argument of perigee: | 275.7543° |
| revolutions per day: | 15.27587559 |
| mean anomaly at epoch: | 84.3112° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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