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 46984U 26145.52153442 +.00000000 +00000-0 +11462-3 0 00005
2 46984 66.0391 182.1298 0007936 270.2737 89.7369 12.80929185 09
| Epoch (UTC): | 25 May 2026 12:31:00 |
| Eccentricity: | 0.0007936 |
| inclination: | 66.0391° |
| perigee height: | 1332 km |
| apogee height: | 1344 km |
| right ascension of ascending node: | 182.1298° |
| argument of perigee: | 270.2737° |
| revolutions per day: | 12.80929185 |
| mean anomaly at epoch: | 89.7369° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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