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 59419U 26145.53558553 +.00000000 +00000-0 +14487-3 0 00005
2 59419 43.0051 342.5965 0002156 274.0262 86.0343 15.27581939 08
| Epoch (UTC): | 25 May 2026 12:51:14 |
| Eccentricity: | 0.0002156 |
| inclination: | 43.0051° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 342.5965° |
| argument of perigee: | 274.0262° |
| revolutions per day: | 15.27581939 |
| mean anomaly at epoch: | 86.0343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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