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 62047U 26145.59558785 +.00000000 +00000-0 +66375-3 0 00002
2 62047 43.0007 189.2420 0002195 282.6494 77.4112 15.27596184 03
| Epoch (UTC): | 25 May 2026 14:17:38 |
| Eccentricity: | 0.0002195 |
| inclination: | 43.0007° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 189.2420° |
| argument of perigee: | 282.6494° |
| revolutions per day: | 15.27596184 |
| mean anomaly at epoch: | 77.4112° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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