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 59200U 26145.00273704 +.00000000 +00000-0 +13077-3 0 00001
2 59200 42.9999 21.4642 0001289 268.6100 91.4604 15.27579376 08
| Epoch (UTC): | 25 May 2026 00:03:56 |
| Eccentricity: | 0.0001289 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 21.4642° |
| argument of perigee: | 268.6100° |
| revolutions per day: | 15.27579376 |
| mean anomaly at epoch: | 91.4604° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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