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 54374U 26145.45418006 +.00000000 +00000-0 +22044-3 0 00007
2 54374 34.9912 148.3444 0009198 306.2318 53.7545 15.20664252 03
| Epoch (UTC): | 25 May 2026 10:54:01 |
| Eccentricity: | 0.0009198 |
| inclination: | 34.9912° |
| perigee height: | 498 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 148.3444° |
| argument of perigee: | 306.2318° |
| revolutions per day: | 15.20664252 |
| mean anomaly at epoch: | 53.7545° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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