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 40015U 26071.03875892 +.00000000 +00000-0 +17652-3 0 00005
2 40015 97.6307 238.0561 0031951 316.3024 43.5662 14.85145410 06
| Epoch (UTC): | 12 March 2026 00:55:48 |
| Eccentricity: | 0.0031951 |
| inclination: | 97.6307° |
| perigee height: | 591 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 238.0561° |
| argument of perigee: | 316.3024° |
| revolutions per day: | 14.85145410 |
| mean anomaly at epoch: | 43.5662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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