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 64118U 26145.58335647 +.00000000 +00000-0 +17100-2 0 00003
2 64118 53.1599 29.4631 0000955 93.8574 31.5947 15.31675229 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000955 |
| inclination: | 53.1599° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 29.4631° |
| argument of perigee: | 93.8574° |
| revolutions per day: | 15.31675229 |
| mean anomaly at epoch: | 31.5947° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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