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 62171U 26145.49700617 +.00000000 +00000-0 +15186-3 0 00006
2 62171 70.0017 330.6539 0002547 261.6042 98.4828 14.98333680 06
| Epoch (UTC): | 25 May 2026 11:55:41 |
| Eccentricity: | 0.0002547 |
| inclination: | 70.0017° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 330.6539° |
| argument of perigee: | 261.6042° |
| revolutions per day: | 14.98333680 |
| mean anomaly at epoch: | 98.4828° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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