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 60235U 26072.63919353 +.00000000 +00000-0 +31611-3 0 00000
2 60235 61.9933 203.4773 0060130 113.5144 247.2280 15.00677283 08
| Epoch (UTC): | 13 March 2026 15:20:26 |
| Eccentricity: | 0.0060130 |
| inclination: | 61.9933° |
| perigee height: | 523 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 203.4773° |
| argument of perigee: | 113.5144° |
| revolutions per day: | 15.00677283 |
| mean anomaly at epoch: | 247.2280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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