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 45700U 26145.64121682 +.00000000 +00000-0 +10048-2 0 00002
2 45700 53.0438 9.6707 0003536 63.0668 297.0706 15.62991002 02
| Epoch (UTC): | 25 May 2026 15:23:21 |
| Eccentricity: | 0.0003536 |
| inclination: | 53.0438° |
| perigee height: | 377 km |
| apogee height: | 381 km |
| right ascension of ascending node: | 9.6707° |
| argument of perigee: | 63.0668° |
| revolutions per day: | 15.62991002 |
| mean anomaly at epoch: | 297.0706° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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