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 37954U 11075A 25268.87846693 0.00000000 00000-0 00000-0 0 09
2 37954 97.5269 340.0855 0001880 355.0565 4.9434 15.17584656 01
| Epoch (UTC): | 25 September 2025 21:04:59 |
| Eccentricity: | 0.0001880 |
| inclination: | 97.5269° |
| perigee height: | 512 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 340.0855° |
| argument of perigee: | 355.0565° |
| revolutions per day: | 15.17584656 |
| mean anomaly at epoch: | 4.9434° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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