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 23432U 26047.05058498 +.00000000 +00000-0 +65941-4 0 00004
2 23432 74.0297 266.4076 0004419 66.7366 85.7019 14.34415398 00
| Epoch (UTC): | 16 February 2026 01:12:50 |
| Eccentricity: | 0.0004419 |
| inclination: | 74.0297° |
| perigee height: | 774 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 266.4076° |
| argument of perigee: | 66.7366° |
| revolutions per day: | 14.34415398 |
| mean anomaly at epoch: | 85.7019° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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