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 41038U 26145.64331992 +.00000000 +00000-0 +11241-3 0 00006
2 41038 98.0045 174.2403 0003018 91.9943 268.1616 14.83064774 06
| Epoch (UTC): | 25 May 2026 15:26:22 |
| Eccentricity: | 0.0003018 |
| inclination: | 98.0045° |
| perigee height: | 618 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 174.2403° |
| argument of perigee: | 91.9943° |
| revolutions per day: | 14.83064774 |
| mean anomaly at epoch: | 268.1616° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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