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 39453U 26079.96457541 +.00000000 +00000-0 +20159-3 0 00002
2 39453 87.3277 87.5577 0003255 95.1877 264.9755 15.48995776 00
| Epoch (UTC): | 20 March 2026 23:08:59 |
| Eccentricity: | 0.0003255 |
| inclination: | 87.3277° |
| perigee height: | 417 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 87.5577° |
| argument of perigee: | 95.1877° |
| revolutions per day: | 15.48995776 |
| mean anomaly at epoch: | 264.9755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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