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 48603U 26145.62059806 +.00000000 +00000-0 +48880-4 0 00000
2 48603 53.1574 116.6569 0000593 96.8008 263.3060 15.29378314 03
| Epoch (UTC): | 25 May 2026 14:53:39 |
| Eccentricity: | 0.0000593 |
| inclination: | 53.1574° |
| perigee height: | 477 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 116.6569° |
| argument of perigee: | 96.8008° |
| revolutions per day: | 15.29378314 |
| mean anomaly at epoch: | 263.3060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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