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 48119U 26145.44705647 +.00000000 +00000-0 +22962-5 0 00007
2 48119 53.1578 155.4127 0001202 84.2557 275.8582 15.31704034 00
| Epoch (UTC): | 25 May 2026 10:43:45 |
| Eccentricity: | 0.0001202 |
| inclination: | 53.1578° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 155.4127° |
| argument of perigee: | 84.2557° |
| revolutions per day: | 15.31704034 |
| mean anomaly at epoch: | 275.8582° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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