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 48644U 26145.24147235 +.00000000 +00000-0 +62266-4 0 00001
2 48644 53.1595 118.0004 0001454 86.9547 273.1621 15.31694352 04
| Epoch (UTC): | 25 May 2026 05:47:43 |
| Eccentricity: | 0.0001454 |
| inclination: | 53.1595° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 118.0004° |
| argument of perigee: | 86.9547° |
| revolutions per day: | 15.31694352 |
| mean anomaly at epoch: | 273.1621° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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