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 64896U 26145.12809161 +.00000000 +00000-0 +27639-3 0 00002
2 64896 97.6698 209.7552 0004710 356.5999 3.5189 14.95138069 00
| Epoch (UTC): | 25 May 2026 03:04:27 |
| Eccentricity: | 0.0004710 |
| inclination: | 97.6698° |
| perigee height: | 579 km |
| apogee height: | 585 km |
| right ascension of ascending node: | 209.7552° |
| argument of perigee: | 356.5999° |
| revolutions per day: | 14.95138069 |
| mean anomaly at epoch: | 3.5189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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