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 62430U 26145.63495804 +.00000000 +00000-0 +87350-4 0 00002
2 62430 97.2789 71.3555 0000990 58.4962 301.6377 15.31944305 09
| Epoch (UTC): | 25 May 2026 15:14:20 |
| Eccentricity: | 0.0000990 |
| inclination: | 97.2789° |
| perigee height: | 469 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 71.3555° |
| argument of perigee: | 58.4962° |
| revolutions per day: | 15.31944305 |
| mean anomaly at epoch: | 301.6377° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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