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 57172U 26121.89654795 +.00000000 +00000-0 +29573-3 0 00009
2 57172 97.5084 180.7822 0011199 281.8340 78.1639 15.20292907 03
| Epoch (UTC): | 01 May 2026 21:31:01 |
| Eccentricity: | 0.0011199 |
| inclination: | 97.5084° |
| perigee height: | 497 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 180.7822° |
| argument of perigee: | 281.8340° |
| revolutions per day: | 15.20292907 |
| mean anomaly at epoch: | 78.1639° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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