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 23230U 26150.53450418 +.00000000 +00000-0 +00000-0 0 00007
2 23230 12.5964 242.0716 5054305 179.6673 162.5532 1.67089847 06
| Epoch (UTC): | 30 May 2026 12:49:41 |
| Eccentricity: | 0.5054305 |
| inclination: | 12.5964° |
| perigee height: | 8458 km |
| apogee height: | 38783 km |
| right ascension of ascending node: | 242.0716° |
| argument of perigee: | 179.6673° |
| revolutions per day: | 1.67089847 |
| mean anomaly at epoch: | 162.5532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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