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 55661U 26145.26319234 +.00000000 +00000-0 +65142-4 0 00006
2 55661 69.9996 331.4214 0002613 270.0624 90.0235 14.98332306 02
| Epoch (UTC): | 25 May 2026 06:18:59 |
| Eccentricity: | 0.0002613 |
| inclination: | 69.9996° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 331.4214° |
| argument of perigee: | 270.0624° |
| revolutions per day: | 14.98332306 |
| mean anomaly at epoch: | 90.0235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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