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 64443U 26145.54777800 +.00000000 +00000-0 +54698-3 0 00005
2 64443 53.1588 91.3036 0000933 87.4395 272.6712 15.30204300 01
| Epoch (UTC): | 25 May 2026 13:08:48 |
| Eccentricity: | 0.0000933 |
| inclination: | 53.1588° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 91.3036° |
| argument of perigee: | 87.4395° |
| revolutions per day: | 15.30204300 |
| mean anomaly at epoch: | 272.6712° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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