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 56164U 26145.31830110 +.00000000 +00000-0 +79932-4 0 00004
2 56164 81.0006 93.7672 0006727 42.2786 317.8887 13.84810611 09
| Epoch (UTC): | 25 May 2026 07:38:21 |
| Eccentricity: | 0.0006727 |
| inclination: | 81.0006° |
| perigee height: | 942 km |
| apogee height: | 952 km |
| right ascension of ascending node: | 93.7672° |
| argument of perigee: | 42.2786° |
| revolutions per day: | 13.84810611 |
| mean anomaly at epoch: | 317.8887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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