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 20466U 26037.79610675 +.00000000 +00000-0 +75621-4 0 00005
2 20466 82.5031 296.4083 0020946 44.8452 315.4451 14.83541772 04
| Epoch (UTC): | 06 February 2026 19:06:23 |
| Eccentricity: | 0.0020946 |
| inclination: | 82.5031° |
| perigee height: | 604 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 296.4083° |
| argument of perigee: | 44.8452° |
| revolutions per day: | 14.83541772 |
| mean anomaly at epoch: | 315.4451° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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