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 48133U 26145.45016031 +.00000000 +00000-0 -21544-3 0 00000
2 48133 53.1581 168.3758 0001349 85.1293 274.9862 15.31667243 03
| Epoch (UTC): | 25 May 2026 10:48:13 |
| Eccentricity: | 0.0001349 |
| inclination: | 53.1581° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 168.3758° |
| argument of perigee: | 85.1293° |
| revolutions per day: | 15.31667243 |
| mean anomaly at epoch: | 274.9862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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