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 59619U 26145.55272837 +.00000000 +00000-0 +65731-4 0 00006
2 59619 43.0024 327.6465 0000466 283.7393 76.3407 15.27580332 02
| Epoch (UTC): | 25 May 2026 13:15:55 |
| Eccentricity: | 0.0000466 |
| inclination: | 43.0024° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 327.6465° |
| argument of perigee: | 283.7393° |
| revolutions per day: | 15.27580332 |
| mean anomaly at epoch: | 76.3407° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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