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 39418U 26118.71599916 +.00000000 +00000-0 +17041-3 0 00009
2 39418 97.3861 169.6887 0023063 123.4890 236.8550 15.12682947 01
| Epoch (UTC): | 28 April 2026 17:11:02 |
| Eccentricity: | 0.0023063 |
| inclination: | 97.3861° |
| perigee height: | 512 km |
| apogee height: | 544 km |
| right ascension of ascending node: | 169.6887° |
| argument of perigee: | 123.4890° |
| revolutions per day: | 15.12682947 |
| mean anomaly at epoch: | 236.8550° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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