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 57353U 26145.10507044 +.00000000 +00000-0 +14795-4 0 00005
2 57353 43.0026 177.3918 0001398 268.5616 91.5076 15.27578682 00
| Epoch (UTC): | 25 May 2026 02:31:18 |
| Eccentricity: | 0.0001398 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 177.3918° |
| argument of perigee: | 268.5616° |
| revolutions per day: | 15.27578682 |
| mean anomaly at epoch: | 91.5076° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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