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 14064U 26157.13851789 +.00000000 +00000-0 +76629-3 0 00004
2 14064 64.9868 87.5699 0039738 201.8748 158.0696 15.38977019 07
| Epoch (UTC): | 06 June 2026 03:19:27 |
| Eccentricity: | 0.0039738 |
| inclination: | 64.9868° |
| perigee height: | 422 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 87.5699° |
| argument of perigee: | 201.8748° |
| revolutions per day: | 15.38977019 |
| mean anomaly at epoch: | 158.0696° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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