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 26114.21357825 +.00000000 +00000-0 +15106-3 0 00009
2 37166 97.9457 92.0133 0020927 97.9312 262.4282 14.91011242 06
| Epoch (UTC): | 24 April 2026 05:07:33 |
| Eccentricity: | 0.0020927 |
| inclination: | 97.9457° |
| perigee height: | 580 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 92.0133° |
| argument of perigee: | 97.9312° |
| revolutions per day: | 14.91011242 |
| mean anomaly at epoch: | 262.4282° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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