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 57168U 26145.61144692 +.00000000 +00000-0 +33441-3 0 00009
2 57168 97.5039 207.8366 0011625 178.2984 181.8296 15.26105478 02
| Epoch (UTC): | 25 May 2026 14:40:29 |
| Eccentricity: | 0.0011625 |
| inclination: | 97.5039° |
| perigee height: | 479 km |
| apogee height: | 495 km |
| right ascension of ascending node: | 207.8366° |
| argument of perigee: | 178.2984° |
| revolutions per day: | 15.26105478 |
| mean anomaly at epoch: | 181.8296° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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