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 48397U 26145.53797439 +.00000000 +00000-0 +42729-4 0 00007
2 48397 53.1595 335.2171 0001029 79.8689 280.2429 15.31701094 00
| Epoch (UTC): | 25 May 2026 12:54:40 |
| Eccentricity: | 0.0001029 |
| inclination: | 53.1595° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 335.2171° |
| argument of perigee: | 79.8689° |
| revolutions per day: | 15.31701094 |
| mean anomaly at epoch: | 280.2429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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