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 48364U 26145.28035639 +.00000000 +00000-0 +25527-4 0 00007
2 48364 53.1600 351.5737 0001256 87.0310 273.0835 15.31699317 09
| Epoch (UTC): | 25 May 2026 06:43:42 |
| Eccentricity: | 0.0001256 |
| inclination: | 53.1600° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 351.5737° |
| argument of perigee: | 87.0310° |
| revolutions per day: | 15.31699317 |
| mean anomaly at epoch: | 273.0835° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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