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 42072U 17015A 25267.89487996 0.00000000 00000-0 00000-0 0 04
2 42072 97.3730 337.8307 0002006 319.1119 40.8880 15.25981528 04
| Epoch (UTC): | 24 September 2025 21:28:37 |
| Eccentricity: | 0.0002006 |
| inclination: | 97.3730° |
| perigee height: | 486 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 337.8307° |
| argument of perigee: | 319.1119° |
| revolutions per day: | 15.25981528 |
| mean anomaly at epoch: | 40.8880° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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