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 39423U 26032.39013343 +.00000000 +00000-0 +18956-3 0 00005
2 39423 97.6978 191.3625 0162673 299.8938 58.6186 14.57750191 03
| Epoch (UTC): | 01 February 2026 09:21:47 |
| Eccentricity: | 0.0162673 |
| inclination: | 97.6978° |
| perigee height: | 585 km |
| apogee height: | 816 km |
| right ascension of ascending node: | 191.3625° |
| argument of perigee: | 299.8938° |
| revolutions per day: | 14.57750191 |
| mean anomaly at epoch: | 58.6186° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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