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 55438U 26145.48733340 +.00000000 +00000-0 +76793-5 0 00005
2 55438 69.9995 230.6449 0003446 270.0412 90.0352 14.98327568 07
| Epoch (UTC): | 25 May 2026 11:41:45 |
| Eccentricity: | 0.0003446 |
| inclination: | 69.9995° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 230.6449° |
| argument of perigee: | 270.0412° |
| revolutions per day: | 14.98327568 |
| mean anomaly at epoch: | 90.0352° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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