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 57367U 26145.44664492 +.00000000 +00000-0 +35759-4 0 00001
2 57367 43.0016 149.5959 0001040 266.9991 93.0742 15.27578848 03
| Epoch (UTC): | 25 May 2026 10:43:10 |
| Eccentricity: | 0.0001040 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 149.5959° |
| argument of perigee: | 266.9991° |
| revolutions per day: | 15.27578848 |
| mean anomaly at epoch: | 93.0742° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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