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 57626U 26145.64198693 +.00000000 +00000-0 +16538-3 0 00009
2 57626 45.0023 62.5677 0005844 167.4242 192.6762 14.60632502 04
| Epoch (UTC): | 25 May 2026 15:24:27 |
| Eccentricity: | 0.0005844 |
| inclination: | 45.0023° |
| perigee height: | 687 km |
| apogee height: | 695 km |
| right ascension of ascending node: | 62.5677° |
| argument of perigee: | 167.4242° |
| revolutions per day: | 14.60632502 |
| mean anomaly at epoch: | 192.6762° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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