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 61597U 26145.37804197 +.00000000 +00000-0 -11262-2 0 00003
2 61597 87.8928 25.5859 0001730 92.4072 267.7254 13.11415717 05
| Epoch (UTC): | 25 May 2026 09:04:22 |
| Eccentricity: | 0.0001730 |
| inclination: | 87.8928° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5859° |
| argument of perigee: | 92.4072° |
| revolutions per day: | 13.11415717 |
| mean anomaly at epoch: | 267.7254° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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