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 39492U 26088.22830704 +.00000000 +00000-0 +14432-3 0 00007
2 39492 82.4192 348.3300 0016497 180.3027 179.8187 14.95839415 04
| Epoch (UTC): | 29 March 2026 05:28:45 |
| Eccentricity: | 0.0016497 |
| inclination: | 82.4192° |
| perigee height: | 568 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 348.3300° |
| argument of perigee: | 180.3027° |
| revolutions per day: | 14.95839415 |
| mean anomaly at epoch: | 179.8187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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