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 60331U 26145.48622133 +.00000000 +00000-0 +32031-4 0 00006
2 60331 53.1606 68.9274 0001095 98.1759 261.9366 15.30196628 00
| Epoch (UTC): | 25 May 2026 11:40:09 |
| Eccentricity: | 0.0001095 |
| inclination: | 53.1606° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 68.9274° |
| argument of perigee: | 98.1759° |
| revolutions per day: | 15.30196628 |
| mean anomaly at epoch: | 261.9366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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