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 64597U 26145.52862559 +.00000000 +00000-0 +68352-3 0 00001
2 64597 53.1615 338.7260 0001342 98.9819 261.1334 15.30196237 04
| Epoch (UTC): | 25 May 2026 12:41:13 |
| Eccentricity: | 0.0001342 |
| inclination: | 53.1615° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.7260° |
| argument of perigee: | 98.9819° |
| revolutions per day: | 15.30196237 |
| mean anomaly at epoch: | 261.1334° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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