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 59237U 26145.50671931 +.00000000 +00000-0 +12887-5 0 00000
2 59237 43.0072 69.7786 0001690 277.1597 82.9063 15.27564018 08
| Epoch (UTC): | 25 May 2026 12:09:40 |
| Eccentricity: | 0.0001690 |
| inclination: | 43.0072° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 69.7786° |
| argument of perigee: | 277.1597° |
| revolutions per day: | 15.27564018 |
| mean anomaly at epoch: | 82.9063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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