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 55296U 26145.54112122 +.00000000 +00000-0 +48740-4 0 00003
2 55296 69.9987 190.5674 0003652 266.5318 93.5424 14.98328913 01
| Epoch (UTC): | 25 May 2026 12:59:12 |
| Eccentricity: | 0.0003652 |
| inclination: | 69.9987° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 190.5674° |
| argument of perigee: | 266.5318° |
| revolutions per day: | 14.98328913 |
| mean anomaly at epoch: | 93.5424° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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