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 61599U 26145.61201101 +.00000000 +00000-0 -15129-2 0 00004
2 61599 87.8927 25.4593 0002157 86.4184 273.7190 13.11414249 06
| Epoch (UTC): | 25 May 2026 14:41:17 |
| Eccentricity: | 0.0002157 |
| inclination: | 87.8927° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.4593° |
| argument of perigee: | 86.4184° |
| revolutions per day: | 13.11414249 |
| mean anomaly at epoch: | 273.7190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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