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 63864U 26145.43300222 +.00000000 +00000-0 +14691-3 0 00008
2 63864 70.0024 41.1656 0002647 269.2947 90.7908 14.98333266 01
| Epoch (UTC): | 25 May 2026 10:23:31 |
| Eccentricity: | 0.0002647 |
| inclination: | 70.0024° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 41.1656° |
| argument of perigee: | 269.2947° |
| revolutions per day: | 14.98333266 |
| mean anomaly at epoch: | 90.7908° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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