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 57166U 26145.61452043 +.00000000 +00000-0 +16193-4 0 00005
2 57166 98.6095 201.0529 0003079 223.0131 137.0808 14.24044560 01
| Epoch (UTC): | 25 May 2026 14:44:54 |
| Eccentricity: | 0.0003079 |
| inclination: | 98.6095° |
| perigee height: | 809 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 201.0529° |
| argument of perigee: | 223.0131° |
| revolutions per day: | 14.24044560 |
| mean anomaly at epoch: | 137.0808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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