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 60989U 26145.44524914 +.00000000 +00000-0 +52394-4 0 00003
2 60989 98.5694 220.5481 0001409 85.5312 274.6032 14.30822603 08
| Epoch (UTC): | 25 May 2026 10:41:09 |
| Eccentricity: | 0.0001409 |
| inclination: | 98.5694° |
| perigee height: | 788 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 220.5481° |
| argument of perigee: | 85.5312° |
| revolutions per day: | 14.30822603 |
| mean anomaly at epoch: | 274.6032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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