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 26016.52708000 +.00000000 +00000-0 +12828-3 0 00000
2 60235 61.9947 38.4543 0063398 100.7643 260.0593 15.00247181 05
| Epoch (UTC): | 16 January 2026 12:38:59 |
| Eccentricity: | 0.0063398 |
| inclination: | 61.9947° |
| perigee height: | 522 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 38.4543° |
| argument of perigee: | 100.7643° |
| revolutions per day: | 15.00247181 |
| mean anomaly at epoch: | 260.0593° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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