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 59895U 26145.01403628 +.00000000 +00000-0 -14104-3 0 00005
2 59895 43.0034 54.0142 0001504 260.9961 99.0720 15.27565335 00
| Epoch (UTC): | 25 May 2026 00:20:12 |
| Eccentricity: | 0.0001504 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 54.0142° |
| argument of perigee: | 260.9961° |
| revolutions per day: | 15.27565335 |
| mean anomaly at epoch: | 99.0720° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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