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 62146U 26144.96258375 +.00000000 +00000-0 +48158-3 0 00003
2 62146 43.0042 87.4713 0001750 286.6550 73.4110 15.27592373 09
| Epoch (UTC): | 24 May 2026 23:06:07 |
| Eccentricity: | 0.0001750 |
| inclination: | 43.0042° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 87.4713° |
| argument of perigee: | 286.6550° |
| revolutions per day: | 15.27592373 |
| mean anomaly at epoch: | 73.4110° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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