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 62744U 26145.55483021 +.00000000 +00000-0 +75623-3 0 00008
2 62744 43.0044 83.6954 0001895 273.0840 86.9795 15.27598762 08
| Epoch (UTC): | 25 May 2026 13:18:57 |
| Eccentricity: | 0.0001895 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 83.6954° |
| argument of perigee: | 273.0840° |
| revolutions per day: | 15.27598762 |
| mean anomaly at epoch: | 86.9795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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