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 26104.15654728 +.00000000 +00000-0 +36988-4 0 00004
2 23179 82.9441 74.5880 0033718 269.0933 101.0613 13.76807239 06
| Epoch (UTC): | 14 April 2026 03:45:25 |
| Eccentricity: | 0.0033718 |
| inclination: | 82.9441° |
| perigee height: | 950 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 74.5880° |
| argument of perigee: | 269.0933° |
| revolutions per day: | 13.76807239 |
| mean anomaly at epoch: | 101.0613° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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