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 59016U 26145.17995176 +.00000000 +00000-0 +34316-4 0 00008
2 59016 53.1612 57.2657 0000919 69.2459 290.8641 15.31705063 08
| Epoch (UTC): | 25 May 2026 04:19:07 |
| Eccentricity: | 0.0000919 |
| inclination: | 53.1612° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 57.2657° |
| argument of perigee: | 69.2459° |
| revolutions per day: | 15.31705063 |
| mean anomaly at epoch: | 290.8641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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