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 59004U 26145.54464391 +.00000000 +00000-0 +15888-3 0 00008
2 59004 53.1595 80.8911 0001487 95.2438 264.8732 15.30168512 00
| Epoch (UTC): | 25 May 2026 13:04:17 |
| Eccentricity: | 0.0001487 |
| inclination: | 53.1595° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 80.8911° |
| argument of perigee: | 95.2438° |
| revolutions per day: | 15.30168512 |
| mean anomaly at epoch: | 264.8732° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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