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 59744U 26145.26448171 +.00000000 +00000-0 +28049-4 0 00000
2 59744 43.0000 110.8370 0000870 263.5897 96.4855 15.27576304 00
| Epoch (UTC): | 25 May 2026 06:20:51 |
| Eccentricity: | 0.0000870 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 110.8370° |
| argument of perigee: | 263.5897° |
| revolutions per day: | 15.27576304 |
| mean anomaly at epoch: | 96.4855° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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