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 57496U 26144.79045851 +.00000000 +00000-0 +13274-3 0 00000
2 57496 43.0026 306.3063 0001484 258.5774 101.4911 15.27569541 06
| Epoch (UTC): | 24 May 2026 18:58:15 |
| Eccentricity: | 0.0001484 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 306.3063° |
| argument of perigee: | 258.5774° |
| revolutions per day: | 15.27569541 |
| mean anomaly at epoch: | 101.4911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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