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 03230U 26071.77098828 +.00000000 +00000-0 +23123-3 0 00000
2 03230 74.0314 307.3983 0023799 129.9519 230.3766 15.03279656 09
| Epoch (UTC): | 12 March 2026 18:30:13 |
| Eccentricity: | 0.0023799 |
| inclination: | 74.0314° |
| perigee height: | 540 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 307.3983° |
| argument of perigee: | 129.9519° |
| revolutions per day: | 15.03279656 |
| mean anomaly at epoch: | 230.3766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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