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 64448U 26145.27080387 +.00000000 +00000-0 +87881-3 0 00007
2 64448 53.1583 93.1327 0001328 92.6411 267.4742 15.30200251 06
| Epoch (UTC): | 25 May 2026 06:29:57 |
| Eccentricity: | 0.0001328 |
| inclination: | 53.1583° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 93.1327° |
| argument of perigee: | 92.6411° |
| revolutions per day: | 15.30200251 |
| mean anomaly at epoch: | 267.4742° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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