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 26145.23001823 +.00000000 +00000-0 +92018-4 0 00006
2 37165 98.3885 10.2476 0033860 317.7639 42.0965 14.82042219 00
| Epoch (UTC): | 25 May 2026 05:31:13 |
| Eccentricity: | 0.0033860 |
| inclination: | 98.3885° |
| perigee height: | 599 km |
| apogee height: | 647 km |
| right ascension of ascending node: | 10.2476° |
| argument of perigee: | 317.7639° |
| revolutions per day: | 14.82042219 |
| mean anomaly at epoch: | 42.0965° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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