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 48648U 26145.61431964 +.00000000 +00000-0 +30175-4 0 00005
2 48648 53.1608 116.2220 0001067 101.8736 258.2385 15.31704543 05
| Epoch (UTC): | 25 May 2026 14:44:37 |
| Eccentricity: | 0.0001067 |
| inclination: | 53.1608° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 116.2220° |
| argument of perigee: | 101.8736° |
| revolutions per day: | 15.31704543 |
| mean anomaly at epoch: | 258.2385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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