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 48662U 26145.23218352 +.00000000 +00000-0 -83145-5 0 00000
2 48662 53.1547 118.3695 0001521 90.4731 269.6443 15.29354982 01
| Epoch (UTC): | 25 May 2026 05:34:20 |
| Eccentricity: | 0.0001521 |
| inclination: | 53.1547° |
| perigee height: | 477 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 118.3695° |
| argument of perigee: | 90.4731° |
| revolutions per day: | 15.29354982 |
| mean anomaly at epoch: | 269.6443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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