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 26032.53108697 +.00000000 +00000-0 +32350-3 0 00004
2 37166 97.9323 9.8685 0020002 12.4529 347.7179 14.90600992 09
| Epoch (UTC): | 01 February 2026 12:44:45 |
| Eccentricity: | 0.0020002 |
| inclination: | 97.9323° |
| perigee height: | 582 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 9.8685° |
| argument of perigee: | 12.4529° |
| revolutions per day: | 14.90600992 |
| mean anomaly at epoch: | 347.7179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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