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 56168U 26145.35913072 +.00000000 +00000-0 +71475-4 0 00005
2 56168 81.0034 93.8514 0012440 50.4794 309.7460 13.84947335 00
| Epoch (UTC): | 25 May 2026 08:37:08 |
| Eccentricity: | 0.0012440 |
| inclination: | 81.0034° |
| perigee height: | 937 km |
| apogee height: | 956 km |
| right ascension of ascending node: | 93.8514° |
| argument of perigee: | 50.4794° |
| revolutions per day: | 13.84947335 |
| mean anomaly at epoch: | 309.7460° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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