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 62162U 26145.53901375 +.00000000 +00000-0 +35714-3 0 00004
2 62162 43.0007 87.5172 0000775 279.2163 80.8601 15.27580657 01
| Epoch (UTC): | 25 May 2026 12:56:10 |
| Eccentricity: | 0.0000775 |
| inclination: | 43.0007° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 87.5172° |
| argument of perigee: | 279.2163° |
| revolutions per day: | 15.27580657 |
| mean anomaly at epoch: | 80.8601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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