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 59900U 26145.43846469 +.00000000 +00000-0 -25617-5 0 00005
2 59900 43.0004 52.0429 0001077 276.3223 83.7506 15.27579604 03
| Epoch (UTC): | 25 May 2026 10:31:23 |
| Eccentricity: | 0.0001077 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 52.0429° |
| argument of perigee: | 276.3223° |
| revolutions per day: | 15.27579604 |
| mean anomaly at epoch: | 83.7506° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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