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 57142U 26145.43653204 +.00000000 +00000-0 +14204-5 0 00003
2 57142 43.0021 189.6724 0001422 311.7241 48.3489 15.27577646 02
| Epoch (UTC): | 25 May 2026 10:28:36 |
| Eccentricity: | 0.0001422 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 189.6724° |
| argument of perigee: | 311.7241° |
| revolutions per day: | 15.27577646 |
| mean anomaly at epoch: | 48.3489° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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