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 57897U 26145.56741148 +.00000000 +00000-0 +58181-4 0 00000
2 57897 43.0009 240.0471 0001519 271.3653 88.7024 15.27570058 04
| Epoch (UTC): | 25 May 2026 13:37:04 |
| Eccentricity: | 0.0001519 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 240.0471° |
| argument of perigee: | 271.3653° |
| revolutions per day: | 15.27570058 |
| mean anomaly at epoch: | 88.7024° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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