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 48434U 26145.41914171 +.00000000 +00000-0 +19656-4 0 00003
2 48434 53.1588 155.9026 0001163 85.7839 274.3295 15.31698886 01
| Epoch (UTC): | 25 May 2026 10:03:33 |
| Eccentricity: | 0.0001163 |
| inclination: | 53.1588° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 155.9026° |
| argument of perigee: | 85.7839° |
| revolutions per day: | 15.31698886 |
| mean anomaly at epoch: | 274.3295° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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