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 64171U 26145.24068586 +.00000000 +00000-0 +85765-3 0 00003
2 64171 53.1579 94.9779 0000965 96.2536 263.8575 15.31719889 05
| Epoch (UTC): | 25 May 2026 05:46:35 |
| Eccentricity: | 0.0000965 |
| inclination: | 53.1579° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 94.9779° |
| argument of perigee: | 96.2536° |
| revolutions per day: | 15.31719889 |
| mean anomaly at epoch: | 263.8575° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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