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 61772U 26145.60502620 +.00000000 +00000-0 +83964-3 0 00008
2 61772 97.2927 24.2780 0004626 23.8612 336.2864 15.69989561 05
| Epoch (UTC): | 25 May 2026 14:31:14 |
| Eccentricity: | 0.0004626 |
| inclination: | 97.2927° |
| perigee height: | 356 km |
| apogee height: | 362 km |
| right ascension of ascending node: | 24.2780° |
| argument of perigee: | 23.8612° |
| revolutions per day: | 15.69989561 |
| mean anomaly at epoch: | 336.2864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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