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 26065.30952602 +.00000000 +00000-0 +31135-3 0 00001
2 60235 61.9928 228.9527 0060792 111.9596 248.7970 15.00610791 01
| Epoch (UTC): | 06 March 2026 07:25:43 |
| Eccentricity: | 0.0060792 |
| inclination: | 61.9928° |
| perigee height: | 523 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 228.9527° |
| argument of perigee: | 111.9596° |
| revolutions per day: | 15.00610791 |
| mean anomaly at epoch: | 248.7970° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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