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 48657U 26145.32068735 +.00000000 +00000-0 +16364-4 0 00009
2 48657 53.1586 117.5419 0001281 86.8476 273.2672 15.31703755 05
| Epoch (UTC): | 25 May 2026 07:41:47 |
| Eccentricity: | 0.0001281 |
| inclination: | 53.1586° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 117.5419° |
| argument of perigee: | 86.8476° |
| revolutions per day: | 15.31703755 |
| mean anomaly at epoch: | 273.2672° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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