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 38736U 26145.50634251 +.00000000 +00000-0 +20142-3 0 00006
2 38736 82.4779 84.9813 0026315 101.0817 259.3224 12.43903317 04
| Epoch (UTC): | 25 May 2026 12:09:07 |
| Eccentricity: | 0.0026315 |
| inclination: | 82.4779° |
| perigee height: | 1469 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 84.9813° |
| argument of perigee: | 101.0817° |
| revolutions per day: | 12.43903317 |
| mean anomaly at epoch: | 259.3224° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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