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 57712U 26145.14061122 +.00000000 +00000-0 +11731-2 0 00005
2 57712 43.0023 46.2460 0001546 278.3976 81.6700 15.27600365 03
| Epoch (UTC): | 25 May 2026 03:22:28 |
| Eccentricity: | 0.0001546 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 46.2460° |
| argument of perigee: | 278.3976° |
| revolutions per day: | 15.27600365 |
| mean anomaly at epoch: | 81.6700° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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