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 57938U 26145.06126439 +.00000000 +00000-0 +39613-4 0 00000
2 57938 53.1609 19.0782 0001201 84.6104 275.5035 15.34390234 03
| Epoch (UTC): | 25 May 2026 01:28:13 |
| Eccentricity: | 0.0001201 |
| inclination: | 53.1609° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 19.0782° |
| argument of perigee: | 84.6104° |
| revolutions per day: | 15.34390234 |
| mean anomaly at epoch: | 275.5035° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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