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 64918U 26144.85712047 +.00000000 +00000-0 +54352-3 0 00004
2 64918 53.1599 351.9997 0000867 81.3351 278.7750 15.33567921 05
| Epoch (UTC): | 24 May 2026 20:34:15 |
| Eccentricity: | 0.0000867 |
| inclination: | 53.1599° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 351.9997° |
| argument of perigee: | 81.3351° |
| revolutions per day: | 15.33567921 |
| mean anomaly at epoch: | 278.7750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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