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 37932U 26045.84853909 +.00000000 +00000-0 +75508-4 0 00009
2 37932 98.8747 0.2806 0035524 251.1420 169.9860 14.22981959 08
| Epoch (UTC): | 14 February 2026 20:21:53 |
| Eccentricity: | 0.0035524 |
| inclination: | 98.8747° |
| perigee height: | 790 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 0.2806° |
| argument of perigee: | 251.1420° |
| revolutions per day: | 14.22981959 |
| mean anomaly at epoch: | 169.9860° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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