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 46266U 26145.51841545 +.00000000 +00000-0 +17975-3 0 00000
2 46266 97.7871 355.8790 0012360 84.6204 275.6429 15.00192005 06
| Epoch (UTC): | 25 May 2026 12:26:31 |
| Eccentricity: | 0.0012360 |
| inclination: | 97.7871° |
| perigee height: | 558 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 355.8790° |
| argument of perigee: | 84.6204° |
| revolutions per day: | 15.00192005 |
| mean anomaly at epoch: | 275.6429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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