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 57106U 26145.52778843 +.00000000 +00000-0 +74219-5 0 00002
2 57106 43.0024 207.6231 0001285 275.7220 84.3485 15.26740051 09
| Epoch (UTC): | 25 May 2026 12:40:00 |
| Eccentricity: | 0.0001285 |
| inclination: | 43.0024° |
| perigee height: | 485 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 207.6231° |
| argument of perigee: | 275.7220° |
| revolutions per day: | 15.26740051 |
| mean anomaly at epoch: | 84.3485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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