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 26073.50540727 +.00000000 +00000-0 +28774-3 0 00008
2 60235 61.9935 200.4664 0060072 113.7140 247.0268 15.00683316 07
| Epoch (UTC): | 14 March 2026 12:07:47 |
| Eccentricity: | 0.0060072 |
| inclination: | 61.9935° |
| perigee height: | 523 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 200.4664° |
| argument of perigee: | 113.7140° |
| revolutions per day: | 15.00683316 |
| mean anomaly at epoch: | 247.0268° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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