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 39442U 26096.97441932 +.00000000 +00000-0 +80054-3 0 00007
2 39442 97.5805 89.6237 0015316 186.9338 173.1693 15.30751597 00
| Epoch (UTC): | 06 April 2026 23:23:09 |
| Eccentricity: | 0.0015316 |
| inclination: | 97.5805° |
| perigee height: | 463 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 89.6237° |
| argument of perigee: | 186.9338° |
| revolutions per day: | 15.30751597 |
| mean anomaly at epoch: | 173.1693° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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