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 57345U 26145.55922095 +.00000000 +00000-0 +31323-4 0 00008
2 57345 43.0015 181.6066 0001944 282.6953 77.3682 15.27576033 02
| Epoch (UTC): | 25 May 2026 13:25:16 |
| Eccentricity: | 0.0001944 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 181.6066° |
| argument of perigee: | 282.6953° |
| revolutions per day: | 15.27576033 |
| mean anomaly at epoch: | 77.3682° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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