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 55397U 26145.45791536 +.00000000 +00000-0 -13158-4 0 00003
2 55397 69.9989 211.0451 0003434 269.5036 90.5730 14.98332468 02
| Epoch (UTC): | 25 May 2026 10:59:23 |
| Eccentricity: | 0.0003434 |
| inclination: | 69.9989° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 211.0451° |
| argument of perigee: | 269.5036° |
| revolutions per day: | 14.98332468 |
| mean anomaly at epoch: | 90.5730° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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