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 48602U 26145.21381194 +.00000000 +00000-0 +45531-4 0 00002
2 48602 53.1576 117.9156 0001294 89.5415 270.5735 15.31704842 01
| Epoch (UTC): | 25 May 2026 05:07:53 |
| Eccentricity: | 0.0001294 |
| inclination: | 53.1576° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 117.9156° |
| argument of perigee: | 89.5415° |
| revolutions per day: | 15.31704842 |
| mean anomaly at epoch: | 270.5735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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