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 48128U 26145.18858719 +.00000000 +00000-0 +23800-2 0 00006
2 48128 53.0985 110.0347 0004044 37.3324 322.7954 15.24274962 09
| Epoch (UTC): | 25 May 2026 04:31:33 |
| Eccentricity: | 0.0004044 |
| inclination: | 53.0985° |
| perigee height: | 490 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 110.0347° |
| argument of perigee: | 37.3324° |
| revolutions per day: | 15.24274962 |
| mean anomaly at epoch: | 322.7954° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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