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 40719U 26071.10032043 +.00000000 +00000-0 +64890-3 0 00003
2 40719 97.5980 289.8024 0012338 202.2673 157.8018 15.02337074 05
| Epoch (UTC): | 12 March 2026 02:24:27 |
| Eccentricity: | 0.0012338 |
| inclination: | 97.5980° |
| perigee height: | 551 km |
| apogee height: | 568 km |
| right ascension of ascending node: | 289.8024° |
| argument of perigee: | 202.2673° |
| revolutions per day: | 15.02337074 |
| mean anomaly at epoch: | 157.8018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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