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 48672U 26145.18355965 +.00000000 +00000-0 +38294-4 0 00000
2 48672 53.1603 108.5382 0001220 75.4369 284.6767 15.31697491 09
| Epoch (UTC): | 25 May 2026 04:24:19 |
| Eccentricity: | 0.0001220 |
| inclination: | 53.1603° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 108.5382° |
| argument of perigee: | 75.4369° |
| revolutions per day: | 15.31697491 |
| mean anomaly at epoch: | 284.6767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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