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 48642U 26145.31636490 +.00000000 +00000-0 +12174-4 0 00006
2 48642 53.1598 117.5405 0001334 87.1822 272.9332 15.31696848 08
| Epoch (UTC): | 25 May 2026 07:35:33 |
| Eccentricity: | 0.0001334 |
| inclination: | 53.1598° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 117.5405° |
| argument of perigee: | 87.1822° |
| revolutions per day: | 15.31696848 |
| mean anomaly at epoch: | 272.9332° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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