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 48679U 26145.63230389 +.00000000 +00000-0 -10655-2 0 00009
2 48679 53.1586 116.4852 0001374 102.9804 257.1350 15.29424785 00
| Epoch (UTC): | 25 May 2026 15:10:31 |
| Eccentricity: | 0.0001374 |
| inclination: | 53.1586° |
| perigee height: | 477 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 116.4852° |
| argument of perigee: | 102.9804° |
| revolutions per day: | 15.29424785 |
| mean anomaly at epoch: | 257.1350° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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