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 48104U 26145.34457569 +.00000000 +00000-0 +22213-5 0 00006
2 48104 53.1591 156.2584 0001227 81.4460 278.6681 15.31699633 03
| Epoch (UTC): | 25 May 2026 08:16:11 |
| Eccentricity: | 0.0001227 |
| inclination: | 53.1591° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 156.2584° |
| argument of perigee: | 81.4460° |
| revolutions per day: | 15.31699633 |
| mean anomaly at epoch: | 278.6681° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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