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 64172U 26145.54836486 +.00000000 +00000-0 +76227-3 0 00002
2 64172 53.1581 94.0518 0001154 74.3568 285.7561 15.31720021 02
| Epoch (UTC): | 25 May 2026 13:09:38 |
| Eccentricity: | 0.0001154 |
| inclination: | 53.1581° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 94.0518° |
| argument of perigee: | 74.3568° |
| revolutions per day: | 15.31720021 |
| mean anomaly at epoch: | 285.7561° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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