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 57155U 26145.48792944 +.00000000 +00000-0 +20167-4 0 00001
2 57155 43.0003 190.0466 0001127 275.6011 84.4712 15.27576208 03
| Epoch (UTC): | 25 May 2026 11:42:37 |
| Eccentricity: | 0.0001127 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 190.0466° |
| argument of perigee: | 275.6011° |
| revolutions per day: | 15.27576208 |
| mean anomaly at epoch: | 84.4712° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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