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 23538U 26071.58943500 +.00000000 +00000-0 +16650-2 0 00004
2 23538 6.4341 263.4001 6043148 209.3987 95.5399 3.96495498 08
| Epoch (UTC): | 12 March 2026 14:08:47 |
| Eccentricity: | 0.6043148 |
| inclination: | 6.4341° |
| perigee height: | 294 km |
| apogee height: | 20674 km |
| right ascension of ascending node: | 263.4001° |
| argument of perigee: | 209.3987° |
| revolutions per day: | 3.96495498 |
| mean anomaly at epoch: | 95.5399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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