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 64885U 26145.57754197 +.00000000 +00000-0 +52926-3 0 00004
2 64885 97.4492 115.8200 0004677 221.3789 138.7102 15.38297251 06
| Epoch (UTC): | 25 May 2026 13:51:39 |
| Eccentricity: | 0.0004677 |
| inclination: | 97.4492° |
| perigee height: | 448 km |
| apogee height: | 454 km |
| right ascension of ascending node: | 115.8200° |
| argument of perigee: | 221.3789° |
| revolutions per day: | 15.38297251 |
| mean anomaly at epoch: | 138.7102° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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