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 64359U 26145.40163434 +.00000000 +00000-0 +34441-3 0 00002
2 64359 70.0004 200.9881 0003714 269.3828 90.6906 14.98328489 07
| Epoch (UTC): | 25 May 2026 09:38:21 |
| Eccentricity: | 0.0003714 |
| inclination: | 70.0004° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 200.9881° |
| argument of perigee: | 269.3828° |
| revolutions per day: | 14.98328489 |
| mean anomaly at epoch: | 90.6906° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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