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 26073.30551219 +.00000000 +00000-0 +28994-3 0 00008
2 60235 61.9934 201.1613 0060091 113.6647 247.0765 15.00681815 04
| Epoch (UTC): | 14 March 2026 07:19:56 |
| Eccentricity: | 0.0060091 |
| inclination: | 61.9934° |
| perigee height: | 523 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 201.1613° |
| argument of perigee: | 113.6647° |
| revolutions per day: | 15.00681815 |
| mean anomaly at epoch: | 247.0765° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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