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 57113U 26145.50992014 +.00000000 +00000-0 +58666-4 0 00003
2 57113 43.0021 207.4911 0001508 268.8515 91.2164 15.27585516 00
| Epoch (UTC): | 25 May 2026 12:14:17 |
| Eccentricity: | 0.0001508 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 207.4911° |
| argument of perigee: | 268.8515° |
| revolutions per day: | 15.27585516 |
| mean anomaly at epoch: | 91.2164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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