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 62739U 26145.53090701 +.00000000 +00000-0 +39664-3 0 00004
2 62739 43.0003 80.0509 0000325 31.9766 328.1105 15.27581688 04
| Epoch (UTC): | 25 May 2026 12:44:30 |
| Eccentricity: | 0.0000325 |
| inclination: | 43.0003° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 80.0509° |
| argument of perigee: | 31.9766° |
| revolutions per day: | 15.27581688 |
| mean anomaly at epoch: | 328.1105° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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