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 46495U 26144.98774177 +.00000000 +00000-0 +24856-3 0 00006
2 46495 97.8855 146.6473 0010594 33.8053 326.3859 15.29404891 03
| Epoch (UTC): | 24 May 2026 23:42:20 |
| Eccentricity: | 0.0010594 |
| inclination: | 97.8855° |
| perigee height: | 470 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 146.6473° |
| argument of perigee: | 33.8053° |
| revolutions per day: | 15.29404891 |
| mean anomaly at epoch: | 326.3859° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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