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 57075U 26145.38044580 +.00000000 +00000-0 +24747-4 0 00005
2 57075 43.0066 22.6387 0001546 281.6401 78.4277 15.27576283 02
| Epoch (UTC): | 25 May 2026 09:07:50 |
| Eccentricity: | 0.0001546 |
| inclination: | 43.0066° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 22.6387° |
| argument of perigee: | 281.6401° |
| revolutions per day: | 15.27576283 |
| mean anomaly at epoch: | 78.4277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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