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 62096U 26144.84970419 +.00000000 +00000-0 +16515-2 0 00005
2 62096 42.9989 303.7840 0001861 270.0497 90.0157 15.70966148 05
| Epoch (UTC): | 24 May 2026 20:23:34 |
| Eccentricity: | 0.0001861 |
| inclination: | 42.9989° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 303.7840° |
| argument of perigee: | 270.0497° |
| revolutions per day: | 15.70966148 |
| mean anomaly at epoch: | 90.0157° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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