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 55433U 26145.34595608 +.00000000 +00000-0 +11232-3 0 00003
2 55433 69.9991 271.0703 0002776 269.1358 90.9483 14.98317380 08
| Epoch (UTC): | 25 May 2026 08:18:10 |
| Eccentricity: | 0.0002776 |
| inclination: | 69.9991° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 271.0703° |
| argument of perigee: | 269.1358° |
| revolutions per day: | 14.98317380 |
| mean anomaly at epoch: | 90.9483° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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