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 62883U 26145.22469074 +.00000000 +00000-0 +18667-2 0 00002
2 62883 43.0001 80.1215 0003735 252.3793 107.6667 15.70982877 00
| Epoch (UTC): | 25 May 2026 05:23:33 |
| Eccentricity: | 0.0003735 |
| inclination: | 43.0001° |
| perigee height: | 354 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 80.1215° |
| argument of perigee: | 252.3793° |
| revolutions per day: | 15.70982877 |
| mean anomaly at epoch: | 107.6667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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