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 57070U 26145.34975691 +.00000000 +00000-0 +13262-4 0 00002
2 57070 43.0016 23.2707 0001032 231.7008 128.3751 15.27576108 02
| Epoch (UTC): | 25 May 2026 08:23:38 |
| Eccentricity: | 0.0001032 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 23.2707° |
| argument of perigee: | 231.7008° |
| revolutions per day: | 15.27576108 |
| mean anomaly at epoch: | 128.3751° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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