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 37165U 26042.06079606 +.00000000 +00000-0 +15209-3 0 00003
2 37165 98.4034 262.0924 0033739 288.2033 71.5507 14.81838597 07
| Epoch (UTC): | 11 February 2026 01:27:32 |
| Eccentricity: | 0.0033739 |
| inclination: | 98.4034° |
| perigee height: | 600 km |
| apogee height: | 647 km |
| right ascension of ascending node: | 262.0924° |
| argument of perigee: | 288.2033° |
| revolutions per day: | 14.81838597 |
| mean anomaly at epoch: | 71.5507° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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