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 26073.83856514 +.00000000 +00000-0 +31965-3 0 00004
2 60235 61.9935 199.3084 0060044 113.7806 246.9596 15.00687077 07
| Epoch (UTC): | 14 March 2026 20:07:32 |
| Eccentricity: | 0.0060044 |
| inclination: | 61.9935° |
| perigee height: | 523 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 199.3084° |
| argument of perigee: | 113.7806° |
| revolutions per day: | 15.00687077 |
| mean anomaly at epoch: | 246.9596° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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