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 39452U 26129.88329492 +.00000000 +00000-0 +15345-3 0 00002
2 39452 87.3322 70.4569 0003519 87.2594 272.9069 15.50172265 03
| Epoch (UTC): | 09 May 2026 21:11:56 |
| Eccentricity: | 0.0003519 |
| inclination: | 87.3322° |
| perigee height: | 414 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 70.4569° |
| argument of perigee: | 87.2594° |
| revolutions per day: | 15.50172265 |
| mean anomaly at epoch: | 272.9069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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