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 26042.25254471 +.00000000 +00000-0 +24872-3 0 00009
2 60235 61.9947 309.0807 0062332 106.7183 254.0760 15.00456508 01
| Epoch (UTC): | 11 February 2026 06:03:39 |
| Eccentricity: | 0.0062332 |
| inclination: | 61.9947° |
| perigee height: | 522 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 309.0807° |
| argument of perigee: | 106.7183° |
| revolutions per day: | 15.00456508 |
| mean anomaly at epoch: | 254.0760° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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