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 57084U 26145.06764360 +.00000000 +00000-0 -11983-3 0 00003
2 57084 43.0053 24.5920 0001711 262.8891 97.1766 15.27596623 01
| Epoch (UTC): | 25 May 2026 01:37:24 |
| Eccentricity: | 0.0001711 |
| inclination: | 43.0053° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 24.5920° |
| argument of perigee: | 262.8891° |
| revolutions per day: | 15.27596623 |
| mean anomaly at epoch: | 97.1766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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