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 37166U 26145.61961689 +.00000000 +00000-0 +18903-3 0 00004
2 37166 97.9467 123.6383 0019454 0.1002 0.0216 14.91119669 05
| Epoch (UTC): | 25 May 2026 14:52:14 |
| Eccentricity: | 0.0019454 |
| inclination: | 97.9467° |
| perigee height: | 581 km |
| apogee height: | 608 km |
| right ascension of ascending node: | 123.6383° |
| argument of perigee: | 0.1002° |
| revolutions per day: | 14.91119669 |
| mean anomaly at epoch: | 0.0216° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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