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 61180U 26144.72139384 +.00000000 +00000-0 +19961-5 0 00004
2 61180 96.6814 36.7957 0004329 46.8146 313.3482 15.75465512 01
| Epoch (UTC): | 24 May 2026 17:18:48 |
| Eccentricity: | 0.0004329 |
| inclination: | 96.6814° |
| perigee height: | 340 km |
| apogee height: | 346 km |
| right ascension of ascending node: | 36.7957° |
| argument of perigee: | 46.8146° |
| revolutions per day: | 15.75465512 |
| mean anomaly at epoch: | 313.3482° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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