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 26139.26361597 +.00000000 +00000-0 +12467-3 0 00002
2 60235 61.9948 331.8386 0054027 129.0328 231.5590 15.00987854 02
| Epoch (UTC): | 19 May 2026 06:19:36 |
| Eccentricity: | 0.0054027 |
| inclination: | 61.9948° |
| perigee height: | 526 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 331.8386° |
| argument of perigee: | 129.0328° |
| revolutions per day: | 15.00987854 |
| mean anomaly at epoch: | 231.5590° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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