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 23533U 26140.56924159 +.00000000 +00000-0 +34527-4 0 00008
2 23533 98.8035 154.7735 0005882 225.3162 231.8995 14.17019277 03
| Epoch (UTC): | 20 May 2026 13:39:42 |
| Eccentricity: | 0.0005882 |
| inclination: | 98.8035° |
| perigee height: | 831 km |
| apogee height: | 840 km |
| right ascension of ascending node: | 154.7735° |
| argument of perigee: | 225.3162° |
| revolutions per day: | 14.17019277 |
| mean anomaly at epoch: | 231.8995° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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