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 60394U 26145.64040654 +.00000000 +00000-0 +14206-3 0 00008
2 60394 88.9715 282.3798 0016661 99.5294 260.7741 13.51006097 08
| Epoch (UTC): | 25 May 2026 15:22:11 |
| Eccentricity: | 0.0016661 |
| inclination: | 88.9715° |
| perigee height: | 1056 km |
| apogee height: | 1081 km |
| right ascension of ascending node: | 282.3798° |
| argument of perigee: | 99.5294° |
| revolutions per day: | 13.51006097 |
| mean anomaly at epoch: | 260.7741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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