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 62168U 26145.52205190 +.00000000 +00000-0 +28904-3 0 00004
2 62168 70.0017 330.7362 0002070 266.9047 93.1876 14.98336766 04
| Epoch (UTC): | 25 May 2026 12:31:45 |
| Eccentricity: | 0.0002070 |
| inclination: | 70.0017° |
| perigee height: | 571 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 330.7362° |
| argument of perigee: | 266.9047° |
| revolutions per day: | 14.98336766 |
| mean anomaly at epoch: | 93.1876° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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