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 59684U 26145.55005583 +.00000000 +00000-0 +47835-3 0 00004
2 59684 42.9994 338.3313 0001961 271.6277 88.4350 15.27553626 04
| Epoch (UTC): | 25 May 2026 13:12:04 |
| Eccentricity: | 0.0001961 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.3313° |
| argument of perigee: | 271.6277° |
| revolutions per day: | 15.27553626 |
| mean anomaly at epoch: | 88.4350° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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