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 48115U 26145.29825221 +.00000000 +00000-0 +23732-4 0 00002
2 48115 53.1589 158.6031 0001357 86.9489 273.1667 15.31698366 06
| Epoch (UTC): | 25 May 2026 07:09:28 |
| Eccentricity: | 0.0001357 |
| inclination: | 53.1589° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 158.6031° |
| argument of perigee: | 86.9489° |
| revolutions per day: | 15.31698366 |
| mean anomaly at epoch: | 273.1667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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