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 40071U 26141.22981472 +.00000000 +00000-0 +14353-3 0 00003
2 40071 98.3857 101.3014 0007467 11.5891 348.5495 14.89888546 02
| Epoch (UTC): | 21 May 2026 05:30:55 |
| Eccentricity: | 0.0007467 |
| inclination: | 98.3857° |
| perigee height: | 593 km |
| apogee height: | 603 km |
| right ascension of ascending node: | 101.3014° |
| argument of perigee: | 11.5891° |
| revolutions per day: | 14.89888546 |
| mean anomaly at epoch: | 348.5495° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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