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 64208U 26145.00462058 +.00000000 +00000-0 +37027-3 0 00008
2 64208 53.1586 44.8637 0001194 78.0882 282.0252 15.30203820 05
| Epoch (UTC): | 25 May 2026 00:06:39 |
| Eccentricity: | 0.0001194 |
| inclination: | 53.1586° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 44.8637° |
| argument of perigee: | 78.0882° |
| revolutions per day: | 15.30203820 |
| mean anomaly at epoch: | 282.0252° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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