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 data is extracted from the following two-line orbital elements,
1 37954U 11075A 25087.89767009 0.00000000 00000-0 00000-0 0 03
2 37954 97.4406 163.4887 0003648 121.6037 238.3961 15.17633269 03
| Epoch (UTC): | 28 March 2025 21:32:38 |
| Eccentricity: | 0.0003648 |
| inclination: | 97.4406° |
| perigee height: | 510 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 163.4887° |
| argument of perigee: | 121.6037° |
| revolutions per day: | 15.17633269 |
| mean anomaly at epoch: | 238.3961° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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