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 55973U 26145.60413064 +.00000000 +00000-0 +28646-3 0 00003
2 55973 97.5230 318.7029 0003605 157.3177 202.8232 15.46550084 09
| Epoch (UTC): | 25 May 2026 14:29:56 |
| Eccentricity: | 0.0003605 |
| inclination: | 97.5230° |
| perigee height: | 424 km |
| apogee height: | 429 km |
| right ascension of ascending node: | 318.7029° |
| argument of perigee: | 157.3177° |
| revolutions per day: | 15.46550084 |
| mean anomaly at epoch: | 202.8232° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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