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 57374U 26145.49675998 +.00000000 +00000-0 +24204-4 0 00000
2 57374 43.0013 149.9878 0001380 266.8833 93.1861 15.27576803 05
| Epoch (UTC): | 25 May 2026 11:55:20 |
| Eccentricity: | 0.0001380 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 149.9878° |
| argument of perigee: | 266.8833° |
| revolutions per day: | 15.27576803 |
| mean anomaly at epoch: | 93.1861° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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