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 26160.21819392 +.00000000 +00000-0 +89470-4 0 00007
2 37165 98.3866 25.9455 0033371 267.9362 91.8027 14.82071176 00
| Epoch (UTC): | 09 June 2026 05:14:11 |
| Eccentricity: | 0.0033371 |
| inclination: | 98.3866° |
| perigee height: | 599 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 25.9455° |
| argument of perigee: | 267.9362° |
| revolutions per day: | 14.82071176 |
| mean anomaly at epoch: | 91.8027° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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