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 56074U 26145.57412155 +.00000000 +00000-0 +17669-3 0 00005
2 56074 87.9000 263.6930 0001507 101.6906 258.4393 13.15549879 09
| Epoch (UTC): | 25 May 2026 13:46:44 |
| Eccentricity: | 0.0001507 |
| inclination: | 87.9000° |
| perigee height: | 1201 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.6930° |
| argument of perigee: | 101.6906° |
| revolutions per day: | 13.15549879 |
| mean anomaly at epoch: | 258.4393° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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