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 48577U 26145.34708615 +.00000000 +00000-0 +27996-3 0 00002
2 48577 53.1587 130.3750 0001314 91.8693 268.2459 15.31709058 01
| Epoch (UTC): | 25 May 2026 08:19:48 |
| Eccentricity: | 0.0001314 |
| inclination: | 53.1587° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 130.3750° |
| argument of perigee: | 91.8693° |
| revolutions per day: | 15.31709058 |
| mean anomaly at epoch: | 268.2459° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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