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 36606U 26088.09587368 +.00000000 +00000-0 +11870-3 0 00004
2 36606 97.4498 27.3578 0420426 121.3514 242.9528 14.28721857 08
| Epoch (UTC): | 29 March 2026 02:18:03 |
| Eccentricity: | 0.0420426 |
| inclination: | 97.4498° |
| perigee height: | 494 km |
| apogee height: | 1098 km |
| right ascension of ascending node: | 27.3578° |
| argument of perigee: | 121.3514° |
| revolutions per day: | 14.28721857 |
| mean anomaly at epoch: | 242.9528° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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