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 26020.19286769 +.00000000 +00000-0 +35898-3 0 00003
2 60235 61.9947 25.7202 0063268 101.5605 259.2597 15.00271716 04
| Epoch (UTC): | 20 January 2026 04:37:43 |
| Eccentricity: | 0.0063268 |
| inclination: | 61.9947° |
| perigee height: | 522 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 25.7202° |
| argument of perigee: | 101.5605° |
| revolutions per day: | 15.00271716 |
| mean anomaly at epoch: | 259.2597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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