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 26067.97489733 +.00000000 +00000-0 +37543-3 0 00005
2 60235 61.9933 219.6890 0060540 112.4958 248.2557 15.00638592 01
| Epoch (UTC): | 08 March 2026 23:23:51 |
| Eccentricity: | 0.0060540 |
| inclination: | 61.9933° |
| perigee height: | 523 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 219.6890° |
| argument of perigee: | 112.4958° |
| revolutions per day: | 15.00638592 |
| mean anomaly at epoch: | 248.2557° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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