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 23179U 26160.20938601 +.00000000 +00000-0 +34751-4 0 00003
2 23179 82.9474 32.9620 0036453 111.2042 8.7475 13.76812029 02
| Epoch (UTC): | 09 June 2026 05:01:30 |
| Eccentricity: | 0.0036453 |
| inclination: | 82.9474° |
| perigee height: | 948 km |
| apogee height: | 1002 km |
| right ascension of ascending node: | 32.9620° |
| argument of perigee: | 111.2042° |
| revolutions per day: | 13.76812029 |
| mean anomaly at epoch: | 8.7475° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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