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 26032.50008536 +.00000000 +00000-0 -51056-3 0 00001
2 38736 82.4817 155.5883 0024416 351.4605 8.6056 12.43898861 00
| Epoch (UTC): | 01 February 2026 12:00:07 |
| Eccentricity: | 0.0024416 |
| inclination: | 82.4817° |
| perigee height: | 1471 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 155.5883° |
| argument of perigee: | 351.4605° |
| revolutions per day: | 12.43898861 |
| mean anomaly at epoch: | 8.6056° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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