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 62996U 26145.14003948 +.00000000 +00000-0 +58858-3 0 00009
2 62996 43.0009 71.9035 0001140 267.9102 92.1619 15.27591448 02
| Epoch (UTC): | 25 May 2026 03:21:39 |
| Eccentricity: | 0.0001140 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 71.9035° |
| argument of perigee: | 267.9102° |
| revolutions per day: | 15.27591448 |
| mean anomaly at epoch: | 92.1619° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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