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 55769U 26145.40992744 +.00000000 +00000-0 -19313-4 0 00004
2 55769 70.0003 31.0774 0002707 270.4687 89.6162 14.98328849 04
| Epoch (UTC): | 25 May 2026 09:50:17 |
| Eccentricity: | 0.0002707 |
| inclination: | 70.0003° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 31.0774° |
| argument of perigee: | 270.4687° |
| revolutions per day: | 14.98328849 |
| mean anomaly at epoch: | 89.6162° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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