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 42738U 26144.59284492 +.00000000 +00000-0 +00000-0 0 00007
2 42738 39.4639 243.5025 0760700 269.0109 83.6451 1.00289926 02
| Epoch (UTC): | 24 May 2026 14:13:41 |
| Eccentricity: | 0.0760700 |
| inclination: | 39.4639° |
| perigee height: | 32574 km |
| apogee height: | 38989 km |
| right ascension of ascending node: | 243.5025° |
| argument of perigee: | 269.0109° |
| revolutions per day: | 1.00289926 |
| mean anomaly at epoch: | 83.6451° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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