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 62747U 26145.10788306 +.00000000 +00000-0 +53201-3 0 00004
2 62747 42.9995 82.8931 0001196 256.7387 103.3332 15.27603406 01
| Epoch (UTC): | 25 May 2026 02:35:21 |
| Eccentricity: | 0.0001196 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 82.8931° |
| argument of perigee: | 256.7387° |
| revolutions per day: | 15.27603406 |
| mean anomaly at epoch: | 103.3332° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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