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 60194U 26145.28384228 +.00000000 +00000-0 +37111-4 0 00005
2 60194 53.1568 143.7017 0001190 85.3444 274.7710 15.69714546 08
| Epoch (UTC): | 25 May 2026 06:48:43 |
| Eccentricity: | 0.0001190 |
| inclination: | 53.1568° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 143.7017° |
| argument of perigee: | 85.3444° |
| revolutions per day: | 15.69714546 |
| mean anomaly at epoch: | 274.7710° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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