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 59942U 26145.04200419 +.00000000 +00000-0 -32201-4 0 00003
2 59942 43.0045 261.0103 0002829 270.0968 89.9560 15.27581746 06
| Epoch (UTC): | 25 May 2026 01:00:29 |
| Eccentricity: | 0.0002829 |
| inclination: | 43.0045° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 261.0103° |
| argument of perigee: | 270.0968° |
| revolutions per day: | 15.27581746 |
| mean anomaly at epoch: | 89.9560° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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