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 42719U 26143.69904294 +.00000000 +00000-0 +00000-0 0 00005
2 42719 63.0598 251.3391 6985086 273.6369 15.8328 2.00884831 09
| Epoch (UTC): | 23 May 2026 16:46:37 |
| Eccentricity: | 0.6985086 |
| inclination: | 63.0598° |
| perigee height: | 1621 km |
| apogee height: | 38687 km |
| right ascension of ascending node: | 251.3391° |
| argument of perigee: | 273.6369° |
| revolutions per day: | 2.00884831 |
| mean anomaly at epoch: | 15.8328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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