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 59849U 26145.55444931 +.00000000 +00000-0 -62392-4 0 00008
2 59849 42.9998 200.1559 0001059 292.9048 67.1692 15.27591380 01
| Epoch (UTC): | 25 May 2026 13:18:24 |
| Eccentricity: | 0.0001059 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.1559° |
| argument of perigee: | 292.9048° |
| revolutions per day: | 15.27591380 |
| mean anomaly at epoch: | 67.1692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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