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 59844U 26145.48520413 +.00000000 +00000-0 +26098-4 0 00007
2 59844 43.0023 200.4954 0001601 268.9908 91.0761 15.27576759 06
| Epoch (UTC): | 25 May 2026 11:38:41 |
| Eccentricity: | 0.0001601 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.4954° |
| argument of perigee: | 268.9908° |
| revolutions per day: | 15.27576759 |
| mean anomaly at epoch: | 91.0761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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