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 48362U 26145.01742943 +.00000000 +00000-0 -16302-4 0 00001
2 48362 53.1615 3.1377 0001125 76.7845 283.3282 15.31695835 07
| Epoch (UTC): | 25 May 2026 00:25:05 |
| Eccentricity: | 0.0001125 |
| inclination: | 53.1615° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 3.1377° |
| argument of perigee: | 76.7845° |
| revolutions per day: | 15.31695835 |
| mean anomaly at epoch: | 283.3282° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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