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 56460U 26145.43820411 +.00000000 +00000-0 -79834-5 0 00002
2 56460 69.9992 310.8868 0002755 266.8342 93.2502 14.98336772 02
| Epoch (UTC): | 25 May 2026 10:31:00 |
| Eccentricity: | 0.0002755 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 310.8868° |
| argument of perigee: | 266.8342° |
| revolutions per day: | 14.98336772 |
| mean anomaly at epoch: | 93.2502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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