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 39073U 26144.85595397 +.00000000 +00000-0 +10933-3 0 00002
2 39073 52.0115 307.6952 0000485 97.9847 262.1075 12.62265217 08
| Epoch (UTC): | 24 May 2026 20:32:34 |
| Eccentricity: | 0.0000485 |
| inclination: | 52.0115° |
| perigee height: | 1413 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 307.6952° |
| argument of perigee: | 97.9847° |
| revolutions per day: | 12.62265217 |
| mean anomaly at epoch: | 262.1075° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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