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 26096.97639734 +.00000000 +00000-0 +26962-3 0 00003
2 39423 97.7097 251.2298 0164718 96.2190 265.7802 14.57971537 04
| Epoch (UTC): | 06 April 2026 23:26:00 |
| Eccentricity: | 0.0164718 |
| inclination: | 97.7097° |
| perigee height: | 583 km |
| apogee height: | 816 km |
| right ascension of ascending node: | 251.2298° |
| argument of perigee: | 96.2190° |
| revolutions per day: | 14.57971537 |
| mean anomaly at epoch: | 265.7802° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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