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 26074.30498531 +.00000000 +00000-0 +26669-3 0 00003
2 60235 61.9936 197.6872 0060019 113.9052 246.8342 15.00689385 03
| Epoch (UTC): | 15 March 2026 07:19:10 |
| Eccentricity: | 0.0060019 |
| inclination: | 61.9936° |
| perigee height: | 523 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 197.6872° |
| argument of perigee: | 113.9052° |
| revolutions per day: | 15.00689385 |
| mean anomaly at epoch: | 246.8342° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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