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 55965U 26145.51051804 +.00000000 +00000-0 +45001-5 0 00000
2 55965 70.0007 70.6280 0002947 270.4665 89.6157 14.98328551 03
| Epoch (UTC): | 25 May 2026 12:15:08 |
| Eccentricity: | 0.0002947 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 70.6280° |
| argument of perigee: | 270.4665° |
| revolutions per day: | 14.98328551 |
| mean anomaly at epoch: | 89.6157° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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