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 56140U 26145.50499088 +.00000000 +00000-0 +38254-4 0 00006
2 56140 43.0047 73.5436 0000973 255.0447 105.0297 15.27572537 08
| Epoch (UTC): | 25 May 2026 12:07:11 |
| Eccentricity: | 0.0000973 |
| inclination: | 43.0047° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 73.5436° |
| argument of perigee: | 255.0447° |
| revolutions per day: | 15.27572537 |
| mean anomaly at epoch: | 105.0297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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