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 57031U 26145.59792671 +.00000000 +00000-0 +46444-3 0 00008
2 57031 97.4924 257.8799 0009639 153.1817 206.9926 15.34088985 08
| Epoch (UTC): | 25 May 2026 14:21:00 |
| Eccentricity: | 0.0009639 |
| inclination: | 97.4924° |
| perigee height: | 457 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 257.8799° |
| argument of perigee: | 153.1817° |
| revolutions per day: | 15.34088985 |
| mean anomaly at epoch: | 206.9926° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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