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 61608U 26145.13051796 +.00000000 +00000-0 +83407-3 0 00009
2 61608 87.8925 25.5706 0000949 108.4230 251.7001 13.11415169 05
| Epoch (UTC): | 25 May 2026 03:07:56 |
| Eccentricity: | 0.0000949 |
| inclination: | 87.8925° |
| perigee height: | 1217 km |
| apogee height: | 1218 km |
| right ascension of ascending node: | 25.5706° |
| argument of perigee: | 108.4230° |
| revolutions per day: | 13.11415169 |
| mean anomaly at epoch: | 251.7001° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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