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 48671U 26145.21059830 +.00000000 +00000-0 -20051-4 0 00008
2 48671 53.1590 118.5295 0001039 75.2730 284.8386 15.29362520 03
| Epoch (UTC): | 25 May 2026 05:03:15 |
| Eccentricity: | 0.0001039 |
| inclination: | 53.1590° |
| perigee height: | 477 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 118.5295° |
| argument of perigee: | 75.2730° |
| revolutions per day: | 15.29362520 |
| mean anomaly at epoch: | 284.8386° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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