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 55940U 26145.55248016 +.00000000 +00000-0 +14164-4 0 00005
2 55940 70.0000 90.6557 0002964 269.8558 90.2261 14.98331694 06
| Epoch (UTC): | 25 May 2026 13:15:34 |
| Eccentricity: | 0.0002964 |
| inclination: | 70.0000° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 90.6557° |
| argument of perigee: | 269.8558° |
| revolutions per day: | 14.98331694 |
| mean anomaly at epoch: | 90.2261° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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