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 40039U 26106.41444198 +.00000000 +00000-0 +61763-4 0 00006
2 40039 97.9603 49.5601 0012483 136.7589 223.4614 14.95423695 04
| Epoch (UTC): | 16 April 2026 09:56:47 |
| Eccentricity: | 0.0012483 |
| inclination: | 97.9603° |
| perigee height: | 572 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 49.5601° |
| argument of perigee: | 136.7589° |
| revolutions per day: | 14.95423695 |
| mean anomaly at epoch: | 223.4614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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