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 59893U 26145.11539095 +.00000000 +00000-0 +10408-3 0 00004
2 59893 42.9984 53.9195 0000687 231.2526 128.8265 15.27579350 02
| Epoch (UTC): | 25 May 2026 02:46:09 |
| Eccentricity: | 0.0000687 |
| inclination: | 42.9984° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 53.9195° |
| argument of perigee: | 231.2526° |
| revolutions per day: | 15.27579350 |
| mean anomaly at epoch: | 128.8265° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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