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 26046.18437764 +.00000000 +00000-0 +19336-3 0 00002
2 60235 61.9945 295.4190 0062132 107.6497 253.1391 15.00478923 03
| Epoch (UTC): | 15 February 2026 04:25:30 |
| Eccentricity: | 0.0062132 |
| inclination: | 61.9945° |
| perigee height: | 522 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 295.4190° |
| argument of perigee: | 107.6497° |
| revolutions per day: | 15.00478923 |
| mean anomaly at epoch: | 253.1391° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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