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 57300U 26145.43256297 +.00000000 +00000-0 -11711-4 0 00000
2 57300 43.0005 149.8145 0001306 267.1896 92.8806 15.27588338 03
| Epoch (UTC): | 25 May 2026 10:22:53 |
| Eccentricity: | 0.0001306 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 149.8145° |
| argument of perigee: | 267.1896° |
| revolutions per day: | 15.27588338 |
| mean anomaly at epoch: | 92.8806° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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