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 26138.13110551 +.00000000 +00000-0 +12893-3 0 00002
2 60235 61.9949 335.7769 0054152 128.7501 231.8447 15.00984557 00
| Epoch (UTC): | 18 May 2026 03:08:47 |
| Eccentricity: | 0.0054152 |
| inclination: | 61.9949° |
| perigee height: | 526 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 335.7769° |
| argument of perigee: | 128.7501° |
| revolutions per day: | 15.00984557 |
| mean anomaly at epoch: | 231.8447° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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