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 00162U 26083.83636466 +.00000000 +00000-0 +73755-4 0 00004
2 00162 47.9005 32.6111 0044143 336.8567 23.0338 14.45360645 01
| Epoch (UTC): | 24 March 2026 20:04:21 |
| Eccentricity: | 0.0044143 |
| inclination: | 47.9005° |
| perigee height: | 709 km |
| apogee height: | 772 km |
| right ascension of ascending node: | 32.6111° |
| argument of perigee: | 336.8567° |
| revolutions per day: | 14.45360645 |
| mean anomaly at epoch: | 23.0338° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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