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 57086U 26145.00997170 +.00000000 +00000-0 +36357-4 0 00008
2 57086 43.0048 25.0127 0001234 264.3135 95.7576 15.27579577 02
| Epoch (UTC): | 25 May 2026 00:14:21 |
| Eccentricity: | 0.0001234 |
| inclination: | 43.0048° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 25.0127° |
| argument of perigee: | 264.3135° |
| revolutions per day: | 15.27579577 |
| mean anomaly at epoch: | 95.7576° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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