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 57195U 26145.58527418 +.00000000 +00000-0 +25784-3 0 00007
2 57195 97.5105 205.2561 0010502 180.4574 179.6653 15.20068421 00
| Epoch (UTC): | 25 May 2026 14:02:47 |
| Eccentricity: | 0.0010502 |
| inclination: | 97.5105° |
| perigee height: | 498 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 205.2561° |
| argument of perigee: | 180.4574° |
| revolutions per day: | 15.20068421 |
| mean anomaly at epoch: | 179.6653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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