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 62165U 26145.46781355 +.00000000 +00000-0 +23103-3 0 00002
2 62165 70.0019 330.9487 0002677 264.9907 95.0946 14.98337459 08
| Epoch (UTC): | 25 May 2026 11:13:39 |
| Eccentricity: | 0.0002677 |
| inclination: | 70.0019° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 330.9487° |
| argument of perigee: | 264.9907° |
| revolutions per day: | 14.98337459 |
| mean anomaly at epoch: | 95.0946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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