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 62738U 26145.53347694 +.00000000 +00000-0 +52154-3 0 00008
2 62738 43.0006 80.0681 0000335 312.3603 47.7220 15.27584760 00
| Epoch (UTC): | 25 May 2026 12:48:12 |
| Eccentricity: | 0.0000335 |
| inclination: | 43.0006° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 80.0681° |
| argument of perigee: | 312.3603° |
| revolutions per day: | 15.27584760 |
| mean anomaly at epoch: | 47.7220° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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