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 17974U 26156.52753580 +.00000000 +00000-0 -53305-4 0 00007
2 17974 71.0074 207.6359 0011694 66.8742 36.2306 14.17655673 00
| Epoch (UTC): | 05 June 2026 12:39:39 |
| Eccentricity: | 0.0011694 |
| inclination: | 71.0074° |
| perigee height: | 825 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 207.6359° |
| argument of perigee: | 66.8742° |
| revolutions per day: | 14.17655673 |
| mean anomaly at epoch: | 36.2306° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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