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 46505U 26144.96808088 +.00000000 +00000-0 +40505-3 0 00004
2 46505 97.8663 149.6052 0007134 71.8687 288.3335 15.41763053 07
| Epoch (UTC): | 24 May 2026 23:14:02 |
| Eccentricity: | 0.0007134 |
| inclination: | 97.8663° |
| perigee height: | 436 km |
| apogee height: | 446 km |
| right ascension of ascending node: | 149.6052° |
| argument of perigee: | 71.8687° |
| revolutions per day: | 15.41763053 |
| mean anomaly at epoch: | 288.3335° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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